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 68795U 26145.34278510 +.00000000 +00000-0 +22150-3 0 00009
2 68795 97.5045 295.2583 0016473 153.9491 206.2570 15.08091164 01
| Epoch (UTC): | 25 May 2026 08:13:36 |
| Eccentricity: | 0.0016473 |
| inclination: | 97.5045° |
| perigee height: | 531 km |
| apogee height: | 553 km |
| right ascension of ascending node: | 295.2583° |
| argument of perigee: | 153.9491° |
| revolutions per day: | 15.08091164 |
| mean anomaly at epoch: | 206.2570° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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