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 64517U 26145.58322970 +.00000000 +00000-0 +48484-3 0 00001
2 64517 51.8989 250.5516 0000461 114.1919 245.9092 14.79943396 02
| Epoch (UTC): | 25 May 2026 13:59:51 |
| Eccentricity: | 0.0000461 |
| inclination: | 51.8989° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 250.5516° |
| argument of perigee: | 114.1919° |
| revolutions per day: | 14.79943396 |
| mean anomaly at epoch: | 245.9092° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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