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 58739U 26145.45227666 +.00000000 +00000-0 +37778-4 0 00007
2 58739 43.0016 146.2186 0000775 261.3057 98.7707 15.27573513 06
| Epoch (UTC): | 25 May 2026 10:51:16 |
| Eccentricity: | 0.0000775 |
| inclination: | 43.0016° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 146.2186° |
| argument of perigee: | 261.3057° |
| revolutions per day: | 15.27573513 |
| mean anomaly at epoch: | 98.7707° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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