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 24277U 26088.13937174 +.00000000 +00000-0 +56134-4 0 00007
2 24277 98.8094 141.5743 0001342 34.9906 325.1363 14.30374435 05
| Epoch (UTC): | 29 March 2026 03:20:41 |
| Eccentricity: | 0.0001342 |
| inclination: | 98.8094° |
| perigee height: | 790 km |
| apogee height: | 791 km |
| right ascension of ascending node: | 141.5743° |
| argument of perigee: | 34.9906° |
| revolutions per day: | 14.30374435 |
| mean anomaly at epoch: | 325.1363° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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