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 36287U 26145.61152615 +.00000000 +00000-0 +00000-0 0 00004
2 36287 4.2431 60.4817 0003092 299.3016 244.0178 1.00272272 01
| Epoch (UTC): | 25 May 2026 14:40:35 |
| Eccentricity: | 0.0003092 |
| inclination: | 4.2431° |
| perigee height: | 35773 km |
| apogee height: | 35800 km |
| right ascension of ascending node: | 60.4817° |
| argument of perigee: | 299.3016° |
| revolutions per day: | 1.00272272 |
| mean anomaly at epoch: | 244.0178° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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