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GRAVITAS

In orbit NORAD 68495 KPDC-5817-0095-1934-1619 United States of America

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

91

Observations all time

Mission information
Spacecraft name
GRAVITAS
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
2026-03-30 11:02:00
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
599.02 km
Apogee
792.49 km
Inclination
97.7°
Period
98.7 min
Semi-major axis
7073.9 km
Velocity
7.43 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-14 14:09:05 UTC
Two-line elements (TLE)
1 68495U 26067CH  26287.25004630  .00123445  00000-0  23097-1 0  9999
2 68495 97.7092 237.7817 0136749 277.7902 205.4576 14.58293318 5432
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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 14:46:51 GRAVITAS
NORAD 68495
METEOR 2-8 DEB
NORAD 36335
4.133 14.84 8.7e-08
2026-10-15 16:04:53 GRAVITAS
NORAD 68495
CZ-3B R/B
NORAD 63525
3.450 13.89 2.3e-07
2026-10-15 19:55:22 GRAVITAS
NORAD 68495
CZ-6A DEB
NORAD 64652
4.292 1.73 2.4e-07
2026-10-16 06:32:01 GRAVITAS
NORAD 68495
SL-14 R/B
NORAD 20466
0.715 15.13 6.8e-06
2026-10-16 21:05:16 KUIPER-00249
NORAD 67154
GRAVITAS
NORAD 68495
3.925 10.59 2.2e-07
2026-10-17 00:29:43 GRAVITAS
NORAD 68495
SL-14 R/B
NORAD 20466
1.784 15.14 1.1e-06
2026-10-17 02:45:02 GRAVITAS
NORAD 68495
IRIDIUM 24
NORAD 25105
3.636 1.72 2.9e-06
2026-10-17 04:07:03 GRAVITAS
NORAD 68495
TITAN 3C TRANSTAGE DEB
NORAD 27721
2.880 12.38 3.4e-07
2026-10-17 13:54:39 GRAVITAS
NORAD 68495
KUIPER-00254
NORAD 68585
3.607 13.14 1.9e-07
2026-10-17 14:14:14 GRAVITAS
NORAD 68495
NOAA 16 DEB
NORAD 41366
4.557 14.77 7.7e-08
2026-10-17 15:34:04 KUIPER-00209
NORAD 67776
GRAVITAS
NORAD 68495
4.399 9.33 1.9e-07
2026-10-18 08:01:18 KUIPER-00061
NORAD 64521
GRAVITAS
NORAD 68495
2.998 10.54 3.7e-07
2026-10-18 13:35:35 GRAVITAS
NORAD 68495
FEDSAT
NORAD 27598
3.755 3.24 3.1e-07
2026-10-19 01:54:03 BEIJING-3B
NORAD 53587
GRAVITAS
NORAD 68495
4.076 13.30 1.5e-07
2026-10-20 06:09:07 TIGRISAT
NORAD 40043
GRAVITAS
NORAD 68495
3.404 14.76 1.5e-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