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 68115U 26145.61799117 +.00000000 +00000-0 +89948-3 0 00004
2 68115 97.2846 106.2582 0001649 98.2734 261.8696 15.33446858 01
| Epoch (UTC): | 25 May 2026 14:49:54 |
| Eccentricity: | 0.0001649 |
| inclination: | 97.2846° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 106.2582° |
| argument of perigee: | 98.2734° |
| revolutions per day: | 15.33446858 |
| mean anomaly at epoch: | 261.8696° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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