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 36108U 26145.51919816 +.00000000 +00000-0 +00000-0 0 00009
2 36108 0.3548 85.7192 0000086 355.5544 218.7582 1.00269712 08
| Epoch (UTC): | 25 May 2026 12:27:38 |
| Eccentricity: | 0.0000086 |
| inclination: | 0.3548° |
| perigee height: | 35787 km |
| apogee height: | 35788 km |
| right ascension of ascending node: | 85.7192° |
| argument of perigee: | 355.5544° |
| revolutions per day: | 1.00269712 |
| mean anomaly at epoch: | 218.7582° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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