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 63883U 26145.42899250 +.00000000 +00000-0 +17091-3 0 00009
2 63883 70.0023 41.1425 0002864 267.6588 92.4243 14.98347416 02
| Epoch (UTC): | 25 May 2026 10:17:44 |
| Eccentricity: | 0.0002864 |
| inclination: | 70.0023° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 41.1425° |
| argument of perigee: | 267.6588° |
| revolutions per day: | 14.98347416 |
| mean anomaly at epoch: | 92.4243° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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