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 68580U 26145.37187535 +.00000000 +00000-0 +11854-2 0 00008
2 68580 51.8746 287.0240 0001688 317.9420 42.1437 15.37264349 07
| Epoch (UTC): | 25 May 2026 08:55:30 |
| Eccentricity: | 0.0001688 |
| inclination: | 51.8746° |
| perigee height: | 453 km |
| apogee height: | 455 km |
| right ascension of ascending node: | 287.0240° |
| argument of perigee: | 317.9420° |
| revolutions per day: | 15.37264349 |
| mean anomaly at epoch: | 42.1437° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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