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Io-1

In orbit NORAD 68498 CINC-4312-3577-0802-5588

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
Io-1
Other names
ACC-IO1
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
586.18 km
Apogee
591.04 km
Inclination
97.8°
Period
96.5 min
Semi-major axis
6966.7 km
Velocity
7.57 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-14 14:09:05 UTC
Two-line elements (TLE)
1 68498U 26067CL  26287.12645327  .00001128  00000-0  11672-3 0  9993
2 68498 97.7699 243.4604 0003488 50.0016 310.1508 14.92035783 29452
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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 11:38:45 IO-1
NORAD 68498
KOYO
NORAD 69916
3.594 7.23 3.1e-07
2026-10-15 17:07:59 IO-1
NORAD 68498
THOR ABLESTAR DEB
NORAD 351
0.506 14.30 7.8e-06
2026-10-16 07:09:02 IO-1
NORAD 68498
DELTA 1 DEB
NORAD 19834
3.356 14.89 1.5e-07
2026-10-16 08:31:58 IO-1
NORAD 68498
IRIDIUM 33 DEB
NORAD 35488
4.276 10.50 1.8e-07
2026-10-16 18:05:54 IO-1
NORAD 68498
THOR ABLESTAR DEB
NORAD 478
4.065 10.49 2.0e-07
2026-10-16 22:06:45 IO-1
NORAD 68498
RUBIN-2 & SAFIR-M
NORAD 27605
4.182 13.68 1.3e-07
2026-10-18 03:09:00 IO-1
NORAD 68498
SCOUT X-4 R/B
NORAD 1815
3.350 13.02 3.1e-07
2026-10-18 05:33:52 IO-1
NORAD 68498
SCOUT X-4 R/B
NORAD 1815
0.777 13.07 5.7e-06
2026-10-18 07:59:25 IO-1
NORAD 68498
PSLV DEB
NORAD 27141
1.983 11.40 7.9e-07
2026-10-19 03:05:07 IO-1
NORAD 68498
ATLAS 28E DEB
NORAD 20565
3.082 1.21 4.6e-07
2026-10-19 08:49:45 TRANSPORTER-14 OBJECT BQ
NORAD 64590
IO-1
NORAD 68498
4.431 14.69 9.1e-08
2026-10-19 09:02:15 IO-1
NORAD 68498
FENGYUN 1C DEB
NORAD 31492
2.610 12.60 4.0e-07
2026-10-19 18:29:18 ARVAKER-3
NORAD 64566
IO-1
NORAD 68498
4.667 14.68 8.2e-08
2026-10-20 02:06:50 NEE-01 PEGASO
NORAD 39151
IO-1
NORAD 68498
3.793 14.88 1.1e-07
2026-10-20 17:21:34 IO-1
NORAD 68498
COSMOS 2251 DEB
NORAD 36050
2.691 4.56 5.8e-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