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 63297U 26145.61193632 +.00000000 +00000-0 +61148-3 0 00002
2 63297 97.6446 288.3023 0007951 224.6057 135.4541 15.24580601 04
| Epoch (UTC): | 25 May 2026 14:41:11 |
| Eccentricity: | 0.0007951 |
| inclination: | 97.6446° |
| perigee height: | 487 km |
| apogee height: | 498 km |
| right ascension of ascending node: | 288.3023° |
| argument of perigee: | 224.6057° |
| revolutions per day: | 15.24580601 |
| mean anomaly at epoch: | 135.4541° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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