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 36508U 26145.61353653 +.00000000 +00000-0 +49820-4 0 00002
2 36508 92.0333 271.8176 0002439 85.0312 275.1174 14.51901177 06
| Epoch (UTC): | 25 May 2026 14:43:29 |
| Eccentricity: | 0.0002439 |
| inclination: | 92.0333° |
| perigee height: | 718 km |
| apogee height: | 721 km |
| right ascension of ascending node: | 271.8176° |
| argument of perigee: | 85.0312° |
| revolutions per day: | 14.51901177 |
| mean anomaly at epoch: | 275.1174° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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