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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
497.00 km
Apogee
497.26 km
Inclination
97.4°
Period
94.6 min
Semi-major axis
6875.3 km
Velocity
7.6 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 04:46:20 UTC
Two-line elements (TLE)
1 66756U 25276CU  26282.64140993  .00006145  00000-0  27307-3 0  9996
2 66756 97.4111 354.6631 0000193 210.2588 149.8637 15.21881577 47837
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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 10:43:46 MAUVE
NORAD 66756
CAS500-2
NORAD 69013
4.863 15.10 6.6e-08
2026-10-11 12:18:29 MAUVE
NORAD 66756
CAS500-2
NORAD 69013
1.019 15.10 1.5e-06
2026-10-11 18:16:15 CONNECTA IOT-9
NORAD 64534
MAUVE
NORAD 66756
2.998 5.41 4.6e-07
2026-10-12 09:16:31 OBJECT C
NORAD 61896
MAUVE
NORAD 66756
2.716 0.59 6.0e-07
2026-10-13 04:00:27 MAUVE
NORAD 66756
TRANSPORTER-15 OBJECT CX
NORAD 66759
0.766 0.00 6.0e-06
2026-10-13 04:20:50 MAUVE
NORAD 66756
TRANSPORTER-15 OBJECT CX
NORAD 66759
0.818 0.00 6.0e-06
2026-10-13 17:25:10 MALLIGYONG-1
NORAD 58400
MAUVE
NORAD 66756
1.672 14.99 5.9e-07
2026-10-14 13:23:52 MAUVE
NORAD 66756
PHOBOS
NORAD 68467
2.817 12.71 3.4e-07
2026-10-14 22:04:34 MAUVE
NORAD 66756
JACK-002
NORAD 68417
4.494 12.71 1.3e-07
2026-10-14 22:51:55 MAUVE
NORAD 66756
JACK-002
NORAD 68417
4.184 12.68 1.6e-07
2026-10-15 07:30:03 FLOCK 4H-3
NORAD 66706
MAUVE
NORAD 66756
3.609 0.02 3.4e-07
2026-10-16 07:57:10 OTTER SDM
NORAD 66678
MAUVE
NORAD 66756
3.234 0.06 4.2e-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