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 68102U 26145.39231509 +.00000000 +00000-0 +66570-3 0 00007
2 68102 97.2821 105.9515 0001161 101.4538 258.6835 15.33451652 07
| Epoch (UTC): | 25 May 2026 09:24:56 |
| Eccentricity: | 0.0001161 |
| inclination: | 97.2821° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 105.9515° |
| argument of perigee: | 101.4538° |
| revolutions per day: | 15.33451652 |
| mean anomaly at epoch: | 258.6835° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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