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 63001U 26145.47596271 +.00000000 +00000-0 +47236-3 0 00007
2 63001 42.9977 70.1217 0001645 269.3991 90.6672 15.27591355 06
| Epoch (UTC): | 25 May 2026 11:25:23 |
| Eccentricity: | 0.0001645 |
| inclination: | 42.9977° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 70.1217° |
| argument of perigee: | 269.3991° |
| revolutions per day: | 15.27591355 |
| mean anomaly at epoch: | 90.6672° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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