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 68879U 26145.29997941 +.00000000 +00000-0 +68384-3 0 00001
2 68879 51.8687 353.3604 0010299 225.4480 134.5665 15.35667651 00
| Epoch (UTC): | 25 May 2026 07:11:58 |
| Eccentricity: | 0.0010299 |
| inclination: | 51.8687° |
| perigee height: | 452 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 353.3604° |
| argument of perigee: | 225.4480° |
| revolutions per day: | 15.35667651 |
| mean anomaly at epoch: | 134.5665° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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