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 63189U 26145.57317145 +.00000000 +00000-0 +12706-2 0 00009
2 63189 43.0015 216.4035 0001790 262.5603 97.5061 15.70853346 04
| Epoch (UTC): | 25 May 2026 13:45:22 |
| Eccentricity: | 0.0001790 |
| inclination: | 43.0015° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 216.4035° |
| argument of perigee: | 262.5603° |
| revolutions per day: | 15.70853346 |
| mean anomaly at epoch: | 97.5061° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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