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FIRESAT1

In orbit NORAD 69886 PVCH-7746-3269-2801-2754

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
FIRESAT1
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
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
597.41 km
Apogee
606.40 km
Inclination
97.8°
Period
96.8 min
Semi-major axis
6980.0 km
Velocity
7.56 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 20:57:00 UTC
Two-line elements (TLE)
1 69886U 26156T   26283.48116680  .00000805  00000-0  94104-4 0  9997
2 69886 97.7895 182.3323 0006541 196.6993 163.4009 14.87781472 14170
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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
2026-10-11 02:57:49 FIRESAT1
NORAD 69886
OBJECT A
NORAD 100609
0.920 14.94 1.9e-06
2026-10-11 23:26:53 FIRESAT1
NORAD 69886
SL-19 R/B
NORAD 36039
0.978 2.01 4.6e-06
2026-10-12 01:48:12 FIRESAT1
NORAD 69886
CZ-6A DEB
NORAD 55888
2.006 13.68 5.7e-07
2026-10-12 07:04:52 FIRESAT1
NORAD 69886
DELTA 1 DEB
NORAD 10346
4.486 8.87 1.8e-07
2026-10-12 10:17:48 FIRESAT1
NORAD 69886
FENGYUN 1C DEB
NORAD 38783
3.340 14.98 1.4e-07
2026-10-12 12:20:09 AETHER-7
NORAD 67378
FIRESAT1
NORAD 69886
2.773 11.26 4.1e-07
2026-10-13 02:06:57 KAZEOSAT 2
NORAD 40010
FIRESAT1
NORAD 69886
4.324 8.08 2.0e-07
2026-10-13 03:05:08 GEESAT-4 04
NORAD 65122
FIRESAT1
NORAD 69886
4.993 12.80 1.1e-07
2026-10-13 20:20:38 WORLDVIEW-3 (WV-3)
NORAD 40115
FIRESAT1
NORAD 69886
4.672 14.95 7.3e-08
2026-10-14 00:37:10 FIRESAT1
NORAD 69886
PEGASUS DEB
NORAD 39322
1.717 15.15 5.0e-07
2026-10-14 01:21:33 FIRESAT1
NORAD 69886
CZ-4B DEB
NORAD 38326
2.314 14.63 3.4e-07
2026-10-14 12:22:31 FIRESAT1
NORAD 69886
CZ-6A DEB
NORAD 55228
2.332 14.96 2.9e-07
2026-10-16 06:52:20 POPACS 2
NORAD 39269
FIRESAT1
NORAD 69886
2.252 15.10 2.9e-07
2026-10-16 08:28:57 POPACS 2
NORAD 39269
FIRESAT1
NORAD 69886
4.002 15.10 9.2e-08
2026-10-16 09:43:05 FIRESAT1
NORAD 69886
CZ-4B DEB
NORAD 26155
3.960 14.95 1.0e-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