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 68300U 26145.52948360 +.00000000 +00000-0 +99717-3 0 00001
2 68300 97.2855 271.8268 0000997 53.1312 307.0044 15.75234486 02
| Epoch (UTC): | 25 May 2026 12:42:27 |
| Eccentricity: | 0.0000997 |
| inclination: | 97.2855° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 271.8268° |
| argument of perigee: | 53.1312° |
| revolutions per day: | 15.75234486 |
| mean anomaly at epoch: | 307.0044° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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