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 68260U 26145.60249242 +.00000000 +00000-0 +87060-3 0 00006
2 68260 53.1579 295.6379 0000956 87.7557 272.3562 15.49327313 09
| Epoch (UTC): | 25 May 2026 14:27:35 |
| Eccentricity: | 0.0000956 |
| inclination: | 53.1579° |
| perigee height: | 418 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 295.6379° |
| argument of perigee: | 87.7557° |
| revolutions per day: | 15.49327313 |
| mean anomaly at epoch: | 272.3562° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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