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 52717U 26145.62842293 +.00000000 +00000-0 +12777-2 0 00005
2 52717 86.0057 107.7092 0046441 100.6612 259.9759 13.29589222 00
| Epoch (UTC): | 25 May 2026 15:04:55 |
| Eccentricity: | 0.0046441 |
| inclination: | 86.0057° |
| perigee height: | 1113 km |
| apogee height: | 1183 km |
| right ascension of ascending node: | 107.7092° |
| argument of perigee: | 100.6612° |
| revolutions per day: | 13.29589222 |
| mean anomaly at epoch: | 259.9759° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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