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 26149.71774270 +.00000000 +00000-0 +00000-0 0 00002
2 02514 17.9484 58.4852 6399129 175.3036 196.2703 2.00346290 07
| Epoch (UTC): | 29 May 2026 17:13:32 |
| Eccentricity: | 0.6399129 |
| inclination: | 17.9484° |
| perigee height: | 3193 km |
| apogee height: | 37210 km |
| right ascension of ascending node: | 58.4852° |
| argument of perigee: | 175.3036° |
| revolutions per day: | 2.00346290 |
| mean anomaly at epoch: | 196.2703° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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