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ARICA-2

In orbit NORAD 68796 IFKU-9201-2588-0809-6295 Japan

Time in UTC

11:53

Next pass · Чукотка · 18°

—

No observations scheduled

40

Observations over 30 days

85%

Successful observations

2k

Frames, latest 2026-10-10 15:28 UTC

Mission information
Spacecraft name
ARICA-2
Call sign
JS1YSD
Status
Active
The satellite is in orbit
Launch and timeline
Carrier rocket
Electron
Spaceport
Rocket Lab Launch Complex 1A
Launch time
2026-04-23 00:00:00
Separation time
2026-04-23 00:00:00
Last observers
Observer
Time of receipt
2026-10-02 13:25:30 UTC
2026-10-02 03:33:18 UTC
2026-10-02 01:59:40 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
524.33 km
Apogee
546.90 km
Inclination
97.5°
Period
95.4 min
Semi-major axis
6913.7 km
Velocity
7.59 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 04:56:40 UTC
Two-line elements (TLE)
1 68796U 26088E   26283.95375883  .00005281  00000-0  33515-3 0  9995
2 68796 97.5226 70.8863 0016323 45.7680 314.4886 15.09204951 25755
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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
2026-10-12 00:52:08 ARICA-2
NORAD 68796
COSMOS 1174 DEB
NORAD 12354
3.893 14.22 1.4e-07
2026-10-12 01:24:20 ARICA-2
NORAD 68796
SAUDISAT 1A (SO-41)
NORAD 26545
2.182 14.23 4.3e-07
2026-10-12 10:18:41 OBJECT A
NORAD 60012
ARICA-2
NORAD 68796
1.649 7.11 1.5e-06
2026-10-12 15:15:56 CANX-2
NORAD 32790
ARICA-2
NORAD 68796
3.755 14.92 1.2e-07
2026-10-14 07:36:34 ARICA-2
NORAD 68796
CZ-4C R/B
NORAD 49123
4.345 10.34 1.8e-07
2026-10-14 20:24:28 COSMOS 2503
NORAD 40420
ARICA-2
NORAD 68796
4.079 10.45 2.0e-07
2026-10-14 22:51:02 ARICA-2
NORAD 68796
OBJECT A
NORAD 100143
4.498 14.21 1.0e-07
2026-10-15 23:13:30 ARICA-2
NORAD 68796
VELOX-PII
NORAD 39438
4.322 14.90 8.9e-08
2026-10-16 00:02:46 ARICA-2
NORAD 68796
SPACEMOBILE-013
NORAD 100240
4.996 9.93 1.4e-07
2026-10-16 00:07:00 ARICA-2
NORAD 68796
IRIDIUM 33 DEB
NORAD 34088
2.601 15.15 2.2e-07
2026-10-16 19:14:08 ARICA-2
NORAD 68796
SL-8 DEB
NORAD 18504
4.873 14.57 8.0e-08

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