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 63244U 26145.26183431 +.00000000 +00000-0 +21996-3 0 00008
2 63244 97.6929 37.0583 0003100 278.4517 81.6352 14.94880281 07
| Epoch (UTC): | 25 May 2026 06:17:02 |
| Eccentricity: | 0.0003100 |
| inclination: | 97.6929° |
| perigee height: | 581 km |
| apogee height: | 585 km |
| right ascension of ascending node: | 37.0583° |
| argument of perigee: | 278.4517° |
| revolutions per day: | 14.94880281 |
| mean anomaly at epoch: | 81.6352° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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