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 65770U 26145.49039362 +.00000000 +00000-0 +11913-2 0 00009
2 65770 51.9012 71.0011 0000920 86.2979 273.8088 14.79925437 04
| Epoch (UTC): | 25 May 2026 11:46:10 |
| Eccentricity: | 0.0000920 |
| inclination: | 51.9012° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 71.0011° |
| argument of perigee: | 86.2979° |
| revolutions per day: | 14.79925437 |
| mean anomaly at epoch: | 273.8088° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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