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 36413U 26145.46076718 +.00000000 +00000-0 +93238-4 0 00006
2 36413 63.3661 57.0285 0535644 21.5615 340.7071 13.45696885 05
| Epoch (UTC): | 25 May 2026 11:03:30 |
| Eccentricity: | 0.0535644 |
| inclination: | 63.3661° |
| perigee height: | 688 km |
| apogee height: | 1488 km |
| right ascension of ascending node: | 57.0285° |
| argument of perigee: | 21.5615° |
| revolutions per day: | 13.45696885 |
| mean anomaly at epoch: | 340.7071° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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