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HOTSAT-2

In orbit NORAD 68465 SFRJ-0541-7202-9133-5119

Observations 0
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Falcon 9 Block 5 | Transporter 16 (Dedicated SSO Rideshare)

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
HOTSAT-2
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Launch
Falcon 9 Block 5 | Transporter 16 (Dedicated SSO Rideshare)
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 4E
Launch time
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
505.77 km
Apogee
511.50 km
Inclination
97.5°
Period
94.9 min
Semi-major axis
6886.8 km
Velocity
7.61 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-14 06:09:05 UTC
Two-line elements (TLE)
1 68465U 26067BB  26286.84094087  .00003486  00000-0  17442-3 0  9996
2 68465  97.4689 243.4859 0004161  46.2988 313.8590 15.18072306 29933
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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 11:11:30 ION SCV-020
NORAD 64545 		HOTSAT-2
NORAD 68465 		3.140 14.75 1.8e-07
2026-10-16 08:46:27 STARLINK-5500
NORAD 55634 		HOTSAT-2
NORAD 68465 		1.955 13.27 2.0e-05
2026-10-16 22:52:22 PVCC
NORAD 58025 		HOTSAT-2
NORAD 68465 		4.565 13.04 1.2e-07
2026-10-17 11:18:45 LEGION 3
NORAD 60452 		HOTSAT-2
NORAD 68465 		3.889 14.08 1.4e-07
2026-10-17 23:25:37 HOTSAT-2
NORAD 68465 		RASSVET-3 32
NORAD 100098 		4.191 12.80 1.5e-07
2026-10-18 00:13:03 HOTSAT-2
NORAD 68465 		RASSVET-3 32
NORAD 100098 		3.934 12.84 1.7e-07
2026-10-18 14:05:40 DB GME UT (DB-GLOBE MISSION EARTH-UT)
NORAD 68459 		HOTSAT-2
NORAD 68465 		4.068 0.00 9.1e-08
2026-10-20 03:21:27 RASSVET-3 2
NORAD 68361 		HOTSAT-2
NORAD 68465 		4.697 2.18 2.0e-07
2026-10-20 04:09:01 RASSVET-3 2
NORAD 68361 		HOTSAT-2
NORAD 68465 		3.963 2.18 2.8e-07
2026-10-20 04:19:33 HOTSAT-2
NORAD 68465 		COSMOS 2251 DEB
NORAD 40794 		4.466 6.76 2.0e-07
2026-10-20 21:47:49 OBJECT C
NORAD 59807 		HOTSAT-2
NORAD 68465 		4.790 12.47 1.2e-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