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 14277U 26064.39444697 +.00000000 +00000-0 +16528-2 0 00002
2 14277 51.9244 78.7617 5399895 103.4453 319.6627 4.93584646 05
| Epoch (UTC): | 05 March 2026 09:28:00 |
| Eccentricity: | 0.5399895 |
| inclination: | 51.9244° |
| perigee height: | 325 km |
| apogee height: | 16061 km |
| right ascension of ascending node: | 78.7617° |
| argument of perigee: | 103.4453° |
| revolutions per day: | 4.93584646 |
| mean anomaly at epoch: | 319.6627° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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