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 68671U 26145.59650435 +.00000000 +00000-0 +48139-3 0 00004
2 68671 97.2863 17.1579 0002158 79.6549 280.4937 15.33449647 00
| Epoch (UTC): | 25 May 2026 14:18:57 |
| Eccentricity: | 0.0002158 |
| inclination: | 97.2863° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 17.1579° |
| argument of perigee: | 79.6549° |
| revolutions per day: | 15.33449647 |
| mean anomaly at epoch: | 280.4937° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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