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TORO-3

In orbit NORAD 68481 BMVG-9246-3923-3953-0918 Taiwan

Time in UTC

—

No observations scheduled

2

Observations over 30 days

91%

Successful observations

11k

Frames, latest 2026-10-12 11:01 UTC

Mission information
Spacecraft name
TORO-3
Status
Active
The satellite is in orbit
Launch and timeline
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 4E
Launch time
2026-03-29 00:00:00
Separation time
2026-03-29 00:00:00
Last observers
Observer
Time of receipt
2026-10-12 11:01:04 UTC
2026-09-24 00:46:29 UTC
2026-09-08 11:07:06 UTC
2026-09-07 10:58:42 UTC
2026-08-29 00:22:01 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
586.73 km
Apogee
588.81 km
Inclination
97.8°
Period
96.5 min
Semi-major axis
6965.9 km
Velocity
7.57 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-13 06:09:06 UTC
Two-line elements (TLE)
1 68481U 26067BT  26285.84995499  .00000687  00000-0  72745-4 0  9998
2 68481 97.7831 242.6606 0001415 305.6319 54.4768 14.92306068 29271
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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
2026-10-14 06:26:34 ION SCV-018
NORAD 64575
TORO-3
NORAD 68481
3.213 14.70 1.7e-07
2026-10-14 06:36:54 TORO-3
NORAD 68481
IRIDE-MS2-HEO-11
NORAD 68983
4.641 7.69 1.8e-07
2026-10-14 14:13:15 TORO-3
NORAD 68481
H-2A DEB
NORAD 38347
4.164 14.98 9.1e-08
2026-10-14 19:19:28 LEMUR-2-HUBBLE-4
NORAD 64565
TORO-3
NORAD 68481
4.483 14.66 8.9e-08
2026-10-14 20:07:43 LEMUR-2-HUBBLE-4
NORAD 64565
TORO-3
NORAD 68481
4.510 14.64 8.8e-08
2026-10-15 01:08:28 TORO-3
NORAD 68481
GSLV R/B
NORAD 54149
4.396 14.64 9.2e-08
2026-10-16 06:52:50 OBJECT G
NORAD 66656
TORO-3
NORAD 68481
1.579 3.78 1.7e-06
2026-10-17 16:35:55 TORO-3
NORAD 68481
OBJECT J
NORAD 44887
4.470 13.38 1.2e-07
2026-10-17 19:53:34 K-HERO
NORAD 66660
TORO-3
NORAD 68481
4.994 3.74 1.7e-07
2026-10-18 01:26:58 TORO-3
NORAD 68481
OBJECT J
NORAD 44887
4.500 13.35 1.2e-07
2026-10-18 03:03:31 TORO-3
NORAD 68481
OBJECT J
NORAD 44887
2.489 13.35 3.9e-07
2026-10-18 04:40:03 TORO-3
NORAD 68481
OBJECT J
NORAD 44887
4.340 13.35 1.3e-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