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 68501U 26145.39363020 +.00000000 +00000-0 +14178-3 0 00001
2 68501 97.7621 103.9826 0004967 97.5821 262.5962 14.91371129 01
| Epoch (UTC): | 25 May 2026 09:26:49 |
| Eccentricity: | 0.0004967 |
| inclination: | 97.7621° |
| perigee height: | 590 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 103.9826° |
| argument of perigee: | 97.5821° |
| revolutions per day: | 14.91371129 |
| mean anomaly at epoch: | 262.5962° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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