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 26142.71889160 +.00000000 +00000-0 +41163-4 0 00009
2 36508 92.0330 271.1148 0002495 85.3373 274.8119 14.51899967 05
| Epoch (UTC): | 22 May 2026 17:15:12 |
| Eccentricity: | 0.0002495 |
| inclination: | 92.0330° |
| perigee height: | 718 km |
| apogee height: | 721 km |
| right ascension of ascending node: | 271.1148° |
| argument of perigee: | 85.3373° |
| revolutions per day: | 14.51899967 |
| mean anomaly at epoch: | 274.8119° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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