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 59072U 26088.16568536 +.00000000 +00000-0 +77647-4 0 00005
2 59072 88.9788 293.5155 0014402 243.9313 116.0409 14.45971469 00
| Epoch (UTC): | 29 March 2026 03:58:35 |
| Eccentricity: | 0.0014402 |
| inclination: | 88.9788° |
| perigee height: | 729 km |
| apogee height: | 749 km |
| right ascension of ascending node: | 293.5155° |
| argument of perigee: | 243.9313° |
| revolutions per day: | 14.45971469 |
| mean anomaly at epoch: | 116.0409° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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