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 58425U 26145.63637713 +.00000000 +00000-0 +80893-4 0 00003
2 58425 49.9600 49.4127 0012878 198.8889 161.1512 13.41495390 04
| Epoch (UTC): | 25 May 2026 15:16:22 |
| Eccentricity: | 0.0012878 |
| inclination: | 49.9600° |
| perigee height: | 1094 km |
| apogee height: | 1113 km |
| right ascension of ascending node: | 49.4127° |
| argument of perigee: | 198.8889° |
| revolutions per day: | 13.41495390 |
| mean anomaly at epoch: | 161.1512° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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