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 68249U 26144.90291742 +.00000000 +00000-0 +62595-3 0 00003
2 68249 53.1590 299.1060 0000850 58.9053 301.2039 15.49336256 06
| Epoch (UTC): | 24 May 2026 21:40:12 |
| Eccentricity: | 0.0000850 |
| inclination: | 53.1590° |
| perigee height: | 418 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 299.1060° |
| argument of perigee: | 58.9053° |
| revolutions per day: | 15.49336256 |
| mean anomaly at epoch: | 301.2039° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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