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 58379U 26145.31918023 +.00000000 +00000-0 +10494-3 0 00001
2 58379 53.1612 4.4371 0001149 99.0169 261.0964 15.34373384 09
| Epoch (UTC): | 25 May 2026 07:39:37 |
| Eccentricity: | 0.0001149 |
| inclination: | 53.1612° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 4.4371° |
| argument of perigee: | 99.0169° |
| revolutions per day: | 15.34373384 |
| mean anomaly at epoch: | 261.0964° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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