RU | EN | ZH --:-- UTC Sign in
Back

HORS 5

In orbit NORAD 67283 GSGJ-8694-0187-1316-8538 Russia

Observations 76
Go to map
Back

Time in UTC

23:13

Next pass · Чукотка · 75°

—

No observations scheduled

1

Observations over 30 days

69%

Successful observations

5

Frames, latest 2026-01-11 15:20 UTC

Mission information
Spacecraft name
HORS 5
Other names
Хорс №5, HORS №5
Network
УниверСат
Status
Active
The satellite is in orbit
Launch and timeline
Launch
Soyuz 2.1b/Fregat-M | AIST-2T 01 & 02
Carrier rocket
Soyuz 2.1b Fregat-M
Upper stage
Фрегат-М
Spaceport
Cosmodrome Site 1S
Launch time
2025-12-28 13:18:05
Separation time
Last observers
Observer
Time of receipt
Сампо-435 [R1NAV]-KP72ab
2026-01-11 15:20:42 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
481.08 km
Apogee
492.76 km
Inclination
97.4°
Period
94.4 min
Semi-major axis
6865.0 km
Velocity
7.61 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-13 22:09:14 UTC
Two-line elements (TLE)
1 67283U 25313AM  26286.42490217  .00006150  00000-0  24696-3 0  9995
2 67283  97.3834 359.7109 0008414 306.5454  53.5009 15.25288856 43986
Copy content
Orbit history, past year

Mean elements of every TLE set over the past 365 days, plotted against the epoch of the set. Each source is its own line; click it in the legend to hide it. A jump in altitude is a manoeuvre or a bad set; lines drifting apart are a disagreement between sources. “TLE age” is how many hours have passed since the epoch of the source's freshest set, plotted against when the set reached us, on a logarithmic scale. A set the source repeats unchanged does not reset the age.

Prediction divergence

Each TLE set is propagated with SGP4 to the epoch of the next set from the same source and compared with it, plotted against the epoch of the next set; the tooltip shows how many hours ahead the prediction ran. The logarithmic scale shows the size of the divergence and the tooltip its sign: plus along-track means the prediction is ahead of the satellite. This is how well the sets agree, not the true error: the reference is a TLE too, off by about a kilometre. An outlier is a manoeuvre between sets. Sets more than a week apart are not compared.

Time of closest approach, UTC Object 1 Object 2 Distance, km Speed, km/s Max. probability
2026-10-15 12:27:53 KSM1-D
NORAD 46907 		HORS 5
NORAD 67283 		4.915 8.88 1.5e-07
2026-10-15 13:44:52 TRANSPORTER-14 OBJECT AE
NORAD 64556 		HORS 5
NORAD 67283 		1.932 5.60 1.1e-06
2026-10-16 20:43:23 KHAYYAM
NORAD 53370 		HORS 5
NORAD 67283 		4.695 15.07 7.2e-08
2026-10-16 22:17:52 KHAYYAM
NORAD 53370 		HORS 5
NORAD 67283 		4.724 15.07 7.1e-08
2026-10-17 01:20:45 SPACEMOBILE-002
NORAD 61048 		HORS 5
NORAD 67283 		1.643 12.24 1.1e-06
2026-10-17 18:38:36 HORS 5
NORAD 67283 		FENGYUN 1C DEB
NORAD 29771 		3.194 14.64 1.8e-07
2026-10-17 19:31:50 HORS 5
NORAD 67283 		STARLINK-36555
NORAD 67497 		4.881 13.55 3.1e-06
2026-10-18 02:45:22 FGN-100-D2
NORAD 66299 		HORS 5
NORAD 67283 		3.843 14.44 1.3e-07
2026-10-18 05:31:40 OBJECT AL
NORAD 67282 		HORS 5
NORAD 67283 		4.083 0.04 2.6e-07
2026-10-18 05:46:25 KANOPUS-V 3
NORAD 43180 		HORS 5
NORAD 67283 		3.149 15.05 1.6e-07
2026-10-18 09:33:59 HORS 5
NORAD 67283 		JIELONG-3 R/B
NORAD 58507 		1.214 15.17 1.0e-06
2026-10-18 13:26:56 HORS 5
NORAD 67283 		TRANSPORTER-16 OBJECT Y
NORAD 68438 		1.962 12.79 7.0e-07
2026-10-19 07:20:58 HORS 5
NORAD 67283 		ZHUQUE-2E R/B
NORAD 69095 		2.388 15.08 2.7e-07

Data: CelesTrak SOCRATES Plus, computed from TLEs of the public catalog. This is an estimate, not grounds for a manoeuvre: TLEs carry no covariance, and the maximum probability assumes a position error.

All conjunctions of this satellite