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 58113U 26145.33630419 +.00000000 +00000-0 +37083-4 0 00003
2 58113 53.1597 169.7230 0001134 81.3166 278.7963 15.30193691 02
| Epoch (UTC): | 25 May 2026 08:04:16 |
| Eccentricity: | 0.0001134 |
| inclination: | 53.1597° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 169.7230° |
| argument of perigee: | 81.3166° |
| revolutions per day: | 15.30193691 |
| mean anomaly at epoch: | 278.7963° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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