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 59007U 26145.09375669 +.00000000 +00000-0 +30637-4 0 00000
2 59007 53.1611 83.0544 0001376 98.2065 261.9092 15.30196378 03
| Epoch (UTC): | 25 May 2026 02:15:00 |
| Eccentricity: | 0.0001376 |
| inclination: | 53.1611° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 83.0544° |
| argument of perigee: | 98.2065° |
| revolutions per day: | 15.30196378 |
| mean anomaly at epoch: | 261.9092° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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