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 68087U 26159.14973486 +.00000000 +00000-0 +79317-3 0 00007
2 68087 53.1595 117.2071 0001328 96.3804 263.7350 15.34399700 09
| Epoch (UTC): | 08 June 2026 03:35:37 |
| Eccentricity: | 0.0001328 |
| inclination: | 53.1595° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 117.2071° |
| argument of perigee: | 96.3804° |
| revolutions per day: | 15.34399700 |
| mean anomaly at epoch: | 263.7350° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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