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 63295U 26145.59409609 +.00000000 +00000-0 +44167-3 0 00003
2 63295 97.6475 285.1121 0013318 207.5677 152.4850 15.16286265 02
| Epoch (UTC): | 25 May 2026 14:15:29 |
| Eccentricity: | 0.0013318 |
| inclination: | 97.6475° |
| perigee height: | 508 km |
| apogee height: | 526 km |
| right ascension of ascending node: | 285.1121° |
| argument of perigee: | 207.5677° |
| revolutions per day: | 15.16286265 |
| mean anomaly at epoch: | 152.4850° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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