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 26066.57803912 +.00000000 +00000-0 +13668-2 0 00009
2 36501 49.6481 286.2942 4795534 84.0463 326.6451 5.96593465 03
| Epoch (UTC): | 07 March 2026 13:52:22 |
| Eccentricity: | 0.4795534 |
| inclination: | 49.6481° |
| perigee height: | 305 km |
| apogee height: | 12622 km |
| right ascension of ascending node: | 286.2942° |
| argument of perigee: | 84.0463° |
| revolutions per day: | 5.96593465 |
| mean anomaly at epoch: | 326.6451° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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