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 02514U 26087.42076251 +.00000000 +00000-0 +00000-0 0 00005
2 02514 17.6668 70.2144 6397187 153.6704 262.5748 2.00370106 06
| Epoch (UTC): | 28 March 2026 10:05:53 |
| Eccentricity: | 0.6397187 |
| inclination: | 17.6668° |
| perigee height: | 3197 km |
| apogee height: | 37201 km |
| right ascension of ascending node: | 70.2144° |
| argument of perigee: | 153.6704° |
| revolutions per day: | 2.00370106 |
| mean anomaly at epoch: | 262.5748° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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