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 65775U 26145.11217902 +.00000000 +00000-0 +10997-3 0 00003
2 65775 51.9035 47.7053 0000792 101.4410 258.6641 14.79932070 04
| Epoch (UTC): | 25 May 2026 02:41:32 |
| Eccentricity: | 0.0000792 |
| inclination: | 51.9035° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 47.7053° |
| argument of perigee: | 101.4410° |
| revolutions per day: | 14.79932070 |
| mean anomaly at epoch: | 258.6641° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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