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

TRYAD-2

In orbit NORAD 66756 GBBQ-0405-2879-6889-6023

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

16

Observations all time

Mission information
Spacecraft name
TRYAD-2
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
2025-11-28 18:44:30
Separation time
2025-11-28 19:39:34
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
496.46 km
Apogee
497.37 km
Inclination
97.4°
Period
94.6 min
Semi-major axis
6875.1 km
Velocity
7.61 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-14 14:09:05 UTC
Two-line elements (TLE)
1 66756U 25276CU  26287.17806478  .00006444  00000-0  28563-3 0  9993
2 66756 97.4098 359.1318 0000663 182.2379 177.8854 15.21951974 48529
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
2026-10-16 04:47:41 OBJECT E
NORAD 61898
MAUVE
NORAD 66756
3.842 0.66 3.0e-07
2026-10-17 15:05:15 GITAI-SC1
NORAD 62388
MAUVE
NORAD 66756
3.052 6.76 4.3e-07
2026-10-17 17:02:47 MAUVE
NORAD 66756
H-2A R/B
NORAD 28932
2.692 11.13 4.4e-07
2026-10-17 20:37:26 CAS500-1
NORAD 47932
MAUVE
NORAD 66756
2.801 15.10 2.0e-07
2026-10-18 06:14:12 HXMT (HUIYAN)
NORAD 42758
MAUVE
NORAD 66756
1.211 13.86 1.5e-06
2026-10-18 11:48:56 MAUVE
NORAD 66756
LPNTSAT-002 (IOD-2)
NORAD 68409
3.588 14.98 1.3e-07
2026-10-19 13:42:44 MAUVE
NORAD 66756
IRIDIUM 33 DEB
NORAD 46971
4.802 15.22 6.4e-08
2026-10-19 14:06:19 MAUVE
NORAD 66756
MARS-1
NORAD 68830
4.599 12.73 1.3e-07
2026-10-20 08:44:02 YAOGAN-36 03B
NORAD 54374
MAUVE
NORAD 66756
2.437 10.02 5.8e-07
2026-10-21 02:21:08 MAUVE
NORAD 66756
SCORPION (RS89S)
NORAD 67293
3.294 0.12 4.1e-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