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 41457U 26150.49257447 +.00000000 +00000-0 +24174-3 0 00001
2 41457 98.2441 163.2601 0001020 99.2616 260.8699 14.59555202 04
| Epoch (UTC): | 30 May 2026 11:49:18 |
| Eccentricity: | 0.0001020 |
| inclination: | 98.2441° |
| perigee height: | 694 km |
| apogee height: | 695 km |
| right ascension of ascending node: | 163.2601° |
| argument of perigee: | 99.2616° |
| revolutions per day: | 14.59555202 |
| mean anomaly at epoch: | 260.8699° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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