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 63072U 26145.50243973 +.00000000 +00000-0 +85277-3 0 00004
2 63072 43.0011 73.5932 0000700 62.0729 298.0194 15.27582596 04
| Epoch (UTC): | 25 May 2026 12:03:30 |
| Eccentricity: | 0.0000700 |
| inclination: | 43.0011° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 73.5932° |
| argument of perigee: | 62.0729° |
| revolutions per day: | 15.27582596 |
| mean anomaly at epoch: | 298.0194° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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