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 36508U 26097.16273931 +.00000000 +00000-0 +73938-4 0 00005
2 36508 92.0259 260.0750 0002475 96.7738 263.3751 14.51899887 06
| Epoch (UTC): | 07 April 2026 03:54:20 |
| Eccentricity: | 0.0002475 |
| inclination: | 92.0259° |
| perigee height: | 718 km |
| apogee height: | 721 km |
| right ascension of ascending node: | 260.0750° |
| argument of perigee: | 96.7738° |
| revolutions per day: | 14.51899887 |
| mean anomaly at epoch: | 263.3751° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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