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 68024U 26145.37012814 +.00000000 +00000-0 +46493-3 0 00006
2 68024 97.2831 94.3663 0001956 67.8995 292.2456 15.33448981 04
| Epoch (UTC): | 25 May 2026 08:52:59 |
| Eccentricity: | 0.0001956 |
| inclination: | 97.2831° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 94.3663° |
| argument of perigee: | 67.8995° |
| revolutions per day: | 15.33448981 |
| mean anomaly at epoch: | 292.2456° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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