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 58940U 26145.16087228 +.00000000 +00000-0 +63517-4 0 00007
2 58940 53.1620 314.6166 0001058 93.5257 266.5865 15.30197986 04
| Epoch (UTC): | 25 May 2026 03:51:39 |
| Eccentricity: | 0.0001058 |
| inclination: | 53.1620° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 314.6166° |
| argument of perigee: | 93.5257° |
| revolutions per day: | 15.30197986 |
| mean anomaly at epoch: | 266.5865° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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