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 26145.62147112 +.00000000 +00000-0 +55277-4 0 00008
2 36798 97.7633 149.1273 0001261 67.9922 292.1421 14.74439964 04
| Epoch (UTC): | 25 May 2026 14:54:55 |
| Eccentricity: | 0.0001261 |
| inclination: | 97.7633° |
| perigee height: | 646 km |
| apogee height: | 648 km |
| right ascension of ascending node: | 149.1273° |
| argument of perigee: | 67.9922° |
| revolutions per day: | 14.74439964 |
| mean anomaly at epoch: | 292.1421° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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