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 26063.05866669 +.00000000 +00000-0 +13339-2 0 00002
2 36501 49.6494 289.6082 4796029 81.2454 328.3211 5.96537433 04
| Epoch (UTC): | 04 March 2026 01:24:28 |
| Eccentricity: | 0.4796029 |
| inclination: | 49.6494° |
| perigee height: | 305 km |
| apogee height: | 12623 km |
| right ascension of ascending node: | 289.6082° |
| argument of perigee: | 81.2454° |
| revolutions per day: | 5.96537433 |
| mean anomaly at epoch: | 328.3211° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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