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 58299U 26145.17816299 +.00000000 +00000-0 +17854-3 0 00005
2 58299 97.3899 228.4111 0006088 220.9720 139.1066 15.34245532 03
| Epoch (UTC): | 25 May 2026 04:16:33 |
| Eccentricity: | 0.0006088 |
| inclination: | 97.3899° |
| perigee height: | 459 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 228.4111° |
| argument of perigee: | 220.9720° |
| revolutions per day: | 15.34245532 |
| mean anomaly at epoch: | 139.1066° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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