HomeManeuver TrackerClose ApproachesSHIYAN 28B-01(SY-28B 01) ⟷ SAPPHIRE
high · CROSS-BORDER
5.30 kmmiss distance
Closest approach (TCA)
2026-09-20 23:34 UTC
Relative speed
7.61 km/s
Altitude
Current separation
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On 2026-09-20 23:34 UTC, CN SHIYAN 28B-01(SY-28B 01) and US SAPPHIRE reached a closest approach (TCA) of 5.30 km, with a relative velocity of 7.61 km/s. This is a cross-border encounter between objects of different nations, the kind of event closely watched for space-security implications. Miss distance and time of closest approach are computed by propagating the latest published orbital elements for both objects, and values update as new element sets are published. See the Satellite Maneuver Tracker for the live picture and space situational awareness for context.

Why it mattersBoth objects are catalogued as payloads. Screening continues as new element sets arrive; operators act on their own conjunction data.

The Two Objects

Dossiers from the satellite directory
NORAD 64753
CountryPRC
Launched2025-07-03
COSPAR2025-145A
Maneuver capableUnknown
SAPPHIREPayload
NORAD 26932
CountryUS
Launched2001-09-30
COSPAR2001-043D
Maneuver capableUnknown

Where This Happens

Altitude context
DEBRIS BELT 700–1000 KM2006001,0001,5002,000 kmTHIS PASS · 790 KMISS 420Starlink 550

At 790 km this pass sits inside the most congested band in low Earth orbit, home to the debris left by the 2007 ASAT test and the 2009 collision. Objects here stay up for decades: there is too little atmospheric drag to clean the band naturally. Why crowded bands matter →

History Between This Pair

1 recorded pass under 10 km
Pair history · SHIYAN 28B-01(SY-28B 01) ⟷ SAPPHIRE
Now5.30 km7.61 km/s790 kmThis page

Repeat encounters are common for objects in near-intersecting orbital planes; each pass is re-screened as fresh element sets arrive.

These Objects Elsewhere

Other screened approaches · 7 days
6.08 km09-19 08:30 UTC
SHIYAN 28B-01(SY-28B 01)SCOUT G-1 R/B
6.96 km09-14 17:41 UTC
OPS 5390SAPPHIRE
7.37 km09-18 06:57 UTC
SHIYAN 28B-01(SY-28B 01)NOAA 16 DEB

How These Numbers Are Computed

Miss distance and TCA come from propagating the latest published orbital elements for both objects and searching for the minimum separation over the screening window. Element sets carry kilometre-scale uncertainty, so figures here describe a close pass, not a collision prediction; a change in either object's published elements re-computes the pass automatically. What is a conjunction? → How conjunction assessment works →

Cite this encounter: Orbital Radar — “SHIYAN 28B-01(SY-28B 01) ⟷ SAPPHIRE: 5.30 km close approach”, https://orbitalradar.com/conjunction/26932-64753 (accessed 2026-09-20).