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 68977U 26145.58335647 +.00000000 +00000-0 -18613-1 0 00000
2 68977 53.1599 267.7411 0001007 77.8460 185.8103 15.69218449 04
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001007 |
| inclination: | 53.1599° |
| perigee height: | 360 km |
| apogee height: | 362 km |
| right ascension of ascending node: | 267.7411° |
| argument of perigee: | 77.8460° |
| revolutions per day: | 15.69218449 |
| mean anomaly at epoch: | 185.8103° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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