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 58939U 26145.48850021 +.00000000 +00000-0 +74493-4 0 00004
2 58939 53.1617 313.1075 0001009 91.9975 268.1141 15.30195754 02
| Epoch (UTC): | 25 May 2026 11:43:26 |
| Eccentricity: | 0.0001009 |
| inclination: | 53.1617° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 313.1075° |
| argument of perigee: | 91.9975° |
| revolutions per day: | 15.30195754 |
| mean anomaly at epoch: | 268.1141° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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