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 00058U 26098.26909948 +.00000000 +00000-0 +36981-4 0 00009
2 00058 28.3263 134.5078 0164889 348.8657 10.8268 13.46428004 01
| Epoch (UTC): | 08 April 2026 06:27:30 |
| Eccentricity: | 0.0164889 |
| inclination: | 28.3263° |
| perigee height: | 962 km |
| apogee height: | 1208 km |
| right ascension of ascending node: | 134.5078° |
| argument of perigee: | 348.8657° |
| revolutions per day: | 13.46428004 |
| mean anomaly at epoch: | 10.8268° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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