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 63300U 26145.61769637 +.00000000 +00000-0 +21832-3 0 00007
2 63300 97.9012 270.1404 0001195 173.0052 187.1173 14.72407463 00
| Epoch (UTC): | 25 May 2026 14:49:28 |
| Eccentricity: | 0.0001195 |
| inclination: | 97.9012° |
| perigee height: | 653 km |
| apogee height: | 654 km |
| right ascension of ascending node: | 270.1404° |
| argument of perigee: | 173.0052° |
| revolutions per day: | 14.72407463 |
| mean anomaly at epoch: | 187.1173° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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