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 36798U 26150.57549206 +.00000000 +00000-0 +21508-3 0 00007
2 36798 97.7622 153.8756 0001184 74.9516 285.1824 14.74452961 02
| Epoch (UTC): | 30 May 2026 13:48:42 |
| Eccentricity: | 0.0001184 |
| inclination: | 97.7622° |
| perigee height: | 646 km |
| apogee height: | 648 km |
| right ascension of ascending node: | 153.8756° |
| argument of perigee: | 74.9516° |
| revolutions per day: | 14.74452961 |
| mean anomaly at epoch: | 285.1824° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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