View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 68002U 26145.54288170 +.00000000 +00000-0 +62770-3 0 00007
2 68002 42.9990 335.2059 0001050 289.6271 70.4467 15.27596023 07
| Epoch (UTC): | 25 May 2026 13:01:44 |
| Eccentricity: | 0.0001050 |
| inclination: | 42.9990° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 335.2059° |
| argument of perigee: | 289.6271° |
| revolutions per day: | 15.27596023 |
| mean anomaly at epoch: | 70.4467° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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