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 36519U 26145.56708632 +.00000000 +00000-0 +45184-4 0 00008
2 36519 82.9601 266.3249 0035992 190.6793 180.9350 13.71664074 02
| Epoch (UTC): | 25 May 2026 13:36:36 |
| Eccentricity: | 0.0035992 |
| inclination: | 82.9601° |
| perigee height: | 967 km |
| apogee height: | 1020 km |
| right ascension of ascending node: | 266.3249° |
| argument of perigee: | 190.6793° |
| revolutions per day: | 13.71664074 |
| mean anomaly at epoch: | 180.9350° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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