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 68317U 26145.33326318 +.00000000 +00000-0 +91026-3 0 00006
2 68317 97.2855 271.6353 0001217 63.2279 296.9111 15.75172270 06
| Epoch (UTC): | 25 May 2026 07:59:53 |
| Eccentricity: | 0.0001217 |
| inclination: | 97.2855° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 271.6353° |
| argument of perigee: | 63.2279° |
| revolutions per day: | 15.75172270 |
| mean anomaly at epoch: | 296.9111° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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