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 36104U 09066A 26008.71074638 0.00004500 00000-0 32159-3 0 02
2 36104 97.3889 11.0536 0002071 142.8443 217.1556 15.04543185 05
| Epoch (UTC): | 08 January 2026 17:03:28 |
| Eccentricity: | 0.0002071 |
| inclination: | 97.3889° |
| perigee height: | 551 km |
| apogee height: | 554 km |
| right ascension of ascending node: | 11.0536° |
| argument of perigee: | 142.8443° |
| revolutions per day: | 15.04543185 |
| mean anomaly at epoch: | 217.1556° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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