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 65168U 26145.63205792 +.00000000 +00000-0 +68139-4 0 00002
2 65168 86.4901 259.4871 0001905 91.2602 268.8750 13.24405977 05
| Epoch (UTC): | 25 May 2026 15:10:09 |
| Eccentricity: | 0.0001905 |
| inclination: | 86.4901° |
| perigee height: | 1167 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 259.4871° |
| argument of perigee: | 91.2602° |
| revolutions per day: | 13.24405977 |
| mean anomaly at epoch: | 268.8750° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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