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 65969U 26145.57127903 +.00000000 +00000-0 +66575-4 0 00003
2 65969 51.9018 355.6361 0000699 108.6136 251.4903 14.79935346 04
| Epoch (UTC): | 25 May 2026 13:42:38 |
| Eccentricity: | 0.0000699 |
| inclination: | 51.9018° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 355.6361° |
| argument of perigee: | 108.6136° |
| revolutions per day: | 14.79935346 |
| mean anomaly at epoch: | 251.4903° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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