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 63868U 26145.42882601 +.00000000 +00000-0 -75374-4 0 00004
2 63868 70.0025 41.1500 0002319 264.4383 95.6511 14.98331202 03
| Epoch (UTC): | 25 May 2026 10:17:30 |
| Eccentricity: | 0.0002319 |
| inclination: | 70.0025° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 41.1500° |
| argument of perigee: | 264.4383° |
| revolutions per day: | 14.98331202 |
| mean anomaly at epoch: | 95.6511° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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