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 68294U 26145.49948563 +.00000000 +00000-0 +20141-2 0 00008
2 68294 97.2842 271.7174 0001979 8.5382 351.5917 15.75221681 03
| Epoch (UTC): | 25 May 2026 11:59:15 |
| Eccentricity: | 0.0001979 |
| inclination: | 97.2842° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 271.7174° |
| argument of perigee: | 8.5382° |
| revolutions per day: | 15.75221681 |
| mean anomaly at epoch: | 351.5917° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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