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 68901U 26145.49176193 +.00000000 +00000-0 +78156-3 0 00005
2 68901 97.2831 341.2632 0002277 97.7195 262.4315 15.49222659 01
| Epoch (UTC): | 25 May 2026 11:48:08 |
| Eccentricity: | 0.0002277 |
| inclination: | 97.2831° |
| perigee height: | 417 km |
| apogee height: | 421 km |
| right ascension of ascending node: | 341.2632° |
| argument of perigee: | 97.7195° |
| revolutions per day: | 15.49222659 |
| mean anomaly at epoch: | 262.4315° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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