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 36501U 26070.59971036 +.00000000 +00000-0 +12533-2 0 00009
2 36501 49.6492 282.5092 4794798 87.2473 324.6291 5.96661336 00
| Epoch (UTC): | 11 March 2026 14:23:34 |
| Eccentricity: | 0.4794798 |
| inclination: | 49.6492° |
| perigee height: | 306 km |
| apogee height: | 12619 km |
| right ascension of ascending node: | 282.5092° |
| argument of perigee: | 87.2473° |
| revolutions per day: | 5.96661336 |
| mean anomaly at epoch: | 324.6291° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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