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 26067.58350473 +.00000000 +00000-0 +13238-2 0 00003
2 36501 49.6480 285.3484 4795345 84.8472 326.1509 5.96610689 08
| Epoch (UTC): | 08 March 2026 14:00:14 |
| Eccentricity: | 0.4795345 |
| inclination: | 49.6480° |
| perigee height: | 305 km |
| apogee height: | 12621 km |
| right ascension of ascending node: | 285.3484° |
| argument of perigee: | 84.8472° |
| revolutions per day: | 5.96610689 |
| mean anomaly at epoch: | 326.1509° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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