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 25344U 26088.04009410 +.00000000 +00000-0 +13606-3 0 00002
2 25344 86.4356 285.8120 0002848 94.7708 265.3823 14.52142056 04
| Epoch (UTC): | 29 March 2026 00:57:44 |
| Eccentricity: | 0.0002848 |
| inclination: | 86.4356° |
| perigee height: | 717 km |
| apogee height: | 721 km |
| right ascension of ascending node: | 285.8120° |
| argument of perigee: | 94.7708° |
| revolutions per day: | 14.52142056 |
| mean anomaly at epoch: | 265.3823° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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