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 58347U 26145.42163576 +.00000000 +00000-0 +00000-0 0 00002
2 58347 0.0521 5.4137 0004580 52.1492 302.4810 5.00116094 01
| Epoch (UTC): | 25 May 2026 10:07:09 |
| Eccentricity: | 0.0004580 |
| inclination: | 0.0521° |
| perigee height: | 8059 km |
| apogee height: | 8072 km |
| right ascension of ascending node: | 5.4137° |
| argument of perigee: | 52.1492° |
| revolutions per day: | 5.00116094 |
| mean anomaly at epoch: | 302.4810° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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