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 26064.19189139 +.00000000 +00000-0 +17288-2 0 00001
2 14277 51.9243 78.8999 5399889 103.3445 319.7414 4.93583044 07
| Epoch (UTC): | 05 March 2026 04:36:19 |
| Eccentricity: | 0.5399889 |
| inclination: | 51.9243° |
| perigee height: | 325 km |
| apogee height: | 16061 km |
| right ascension of ascending node: | 78.8999° |
| argument of perigee: | 103.3445° |
| revolutions per day: | 4.93583044 |
| mean anomaly at epoch: | 319.7414° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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