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 68279U 26145.49669425 +.00000000 +00000-0 +11514-2 0 00002
2 68279 53.1595 321.5733 0001180 72.6632 287.4500 15.35431540 09
| Epoch (UTC): | 25 May 2026 11:55:14 |
| Eccentricity: | 0.0001180 |
| inclination: | 53.1595° |
| perigee height: | 459 km |
| apogee height: | 460 km |
| right ascension of ascending node: | 321.5733° |
| argument of perigee: | 72.6632° |
| revolutions per day: | 15.35431540 |
| mean anomaly at epoch: | 287.4500° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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