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 58328U 26145.22008409 +.00000000 +00000-0 +39232-3 0 00004
2 58328 97.3998 235.3823 0005669 215.8834 144.2037 15.50548170 03
| Epoch (UTC): | 25 May 2026 05:16:55 |
| Eccentricity: | 0.0005669 |
| inclination: | 97.3998° |
| perigee height: | 411 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 235.3823° |
| argument of perigee: | 215.8834° |
| revolutions per day: | 15.50548170 |
| mean anomaly at epoch: | 144.2037° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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