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 65968U 26145.33222128 +.00000000 +00000-0 +30945-3 0 00002
2 65968 51.9021 359.1956 0000818 115.5394 244.5653 14.79936203 00
| Epoch (UTC): | 25 May 2026 07:58:23 |
| Eccentricity: | 0.0000818 |
| inclination: | 51.9021° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 359.1956° |
| argument of perigee: | 115.5394° |
| revolutions per day: | 14.79936203 |
| mean anomaly at epoch: | 244.5653° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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