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 25544U 26064.25394532 +.00000000 +00000-0 +16717-3 0 00009
2 25544 51.6314 94.2866 0008161 158.8383 201.2944 15.48454548 09
| Epoch (UTC): | 05 March 2026 06:05:40 |
| Eccentricity: | 0.0008161 |
| inclination: | 51.6314° |
| perigee height: | 416 km |
| apogee height: | 427 km |
| right ascension of ascending node: | 94.2866° |
| argument of perigee: | 158.8383° |
| revolutions per day: | 15.48454548 |
| mean anomaly at epoch: | 201.2944° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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