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

SPEQTRE

In orbit NORAD 66769 FOHT-7729-6464-9363-1679

Falcon 9

Carrier rocket

База Вандерберг

Spaceport

0

Observations all time

Mission information
Spacecraft name
SPEQTRE
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
Spaceport
База Вандерберг
Launch time
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
497.42 km
Apogee
500.14 km
Inclination
97.4°
Period
94.7 min
Semi-major axis
6876.9 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 66769U 25276DH  26282.96535544  .00004328  00000-0  19636-3 0  9992
2 66769 97.4109 354.9985 0001976 133.3398 226.8002 15.21334381 47880
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
2026-10-10 17:44:09 QB50P1
NORAD 40025
SPEQTRE
NORAD 66769
4.425 6.67 2.1e-07
2026-10-11 01:46:18 SPEQTRE
NORAD 66769
SL-24 R/B
NORAD 36606
4.247 15.00 9.5e-08
2026-10-11 17:37:33 KANOPUS-V 4
NORAD 43181
SPEQTRE
NORAD 66769
3.733 15.01 1.2e-07
2026-10-11 19:59:34 KANOPUS-V 4
NORAD 43181
SPEQTRE
NORAD 66769
2.998 15.04 1.8e-07
2026-10-14 14:04:23 RAISE 2
NORAD 49397
SPEQTRE
NORAD 66769
2.164 5.42 8.9e-07
2026-10-15 14:54:39 CAS500-1
NORAD 47932
SPEQTRE
NORAD 66769
1.601 15.10 6.1e-07
2026-10-15 16:29:24 CAS500-1
NORAD 47932
SPEQTRE
NORAD 66769
2.890 15.10 1.9e-07
2026-10-15 21:12:29 CHAMRAN-1
NORAD 61072
SPEQTRE
NORAD 66769
1.412 4.40 2.1e-06
2026-10-16 05:31:41 CARTOSAT-3
NORAD 44804
SPEQTRE
NORAD 66769
4.044 1.59 2.7e-07
2026-10-16 06:44:36 SEMI-1N
NORAD 66297
SPEQTRE
NORAD 66769
1.985 14.41 5.1e-07
2026-10-16 09:54:10 SEMI-1P
NORAD 66298
SPEQTRE
NORAD 66769
4.708 14.40 9.0e-08
2026-10-16 12:40:41 SPEQTRE
NORAD 66769
TRANSPORTER-16 OBJECT L
NORAD 68426
3.317 12.67 2.5e-07
2026-10-16 13:12:51 MALLIGYONG-1
NORAD 58400
SPEQTRE
NORAD 66769
1.777 14.99 5.2e-07
2026-10-16 13:28:01 SPEQTRE
NORAD 66769
TRANSPORTER-16 OBJECT L
NORAD 68426
2.608 12.70 4.0e-07
2026-10-17 00:06:17 TOMORROW-S9
NORAD 66309
SPEQTRE
NORAD 66769
3.341 14.42 1.8e-07
2026-10-17 01:48:09 HXMT (HUIYAN)
NORAD 42758
SPEQTRE
NORAD 66769
3.605 13.62 1.8e-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