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 63235U 26088.15875470 +.00000000 +00000-0 +44952-3 0 00000
2 63235 97.3967 341.8064 0008346 85.1620 275.0570 15.22817717 08
| Epoch (UTC): | 29 March 2026 03:48:36 |
| Eccentricity: | 0.0008346 |
| inclination: | 97.3967° |
| perigee height: | 492 km |
| apogee height: | 503 km |
| right ascension of ascending node: | 341.8064° |
| argument of perigee: | 85.1620° |
| revolutions per day: | 15.22817717 |
| mean anomaly at epoch: | 275.0570° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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