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ARQSAT-1

In orbit NORAD 68419 JIKH-1381-0513-1618-0623 Spain

Time in UTC

—

No observations scheduled

1

Observations over 30 days

70%

Successful observations

2k

Frames, latest 2026-10-03 22:11 UTC

Mission information
Spacecraft name
ARQSAT-1
Other names
FEMTO-1
Status
Active
The satellite is in orbit
Launch and timeline
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 4E
Launch time
2026-03-30 11:02:00
Separation time
Last observers
Observer
Time of receipt
2026-09-17 11:09:11 UTC
2026-06-17 12:16:44 UTC
2026-06-17 01:28:43 UTC
2026-06-15 11:20:23 UTC
2026-06-15 02:06:14 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
503.10 km
Apogee
505.41 km
Inclination
97.5°
Period
94.8 min
Semi-major axis
6882.4 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 68419U 26067D   26287.19132153  .00002970  00000-0  14306-3 0  9994
2 68419 97.4702 244.2720 0001682 145.0783 215.0562 15.19521613 30014
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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 11:20:35 OBJECT F
NORAD 63296
FEMTO-1
NORAD 68419
1.848 15.08 4.6e-07
2026-10-15 12:55:27 OBJECT F
NORAD 63296
FEMTO-1
NORAD 68419
4.129 15.08 9.2e-08
2026-10-16 10:51:11 FEMTO-1
NORAD 68419
SL-4 R/B
NORAD 68753
4.626 14.66 8.6e-08
2026-10-17 11:56:41 FEMTO-1
NORAD 68419
TABLETSAT-AURORA
NORAD 40017
3.573 13.35 1.9e-07
2026-10-19 23:59:09 FEMTO-1
NORAD 68419
COSMOS 2251 DEB
NORAD 37316
4.790 14.59 8.3e-08
2026-10-20 23:47:21 FEMTO-1
NORAD 68419
GEN1A-2
NORAD 69005
2.691 7.72 5.4e-07
2026-10-21 02:53:10 OBJECT D
NORAD 66056
FEMTO-1
NORAD 68419
4.149 12.28 1.7e-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