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 62854U 26145.34322368 +.00000000 +00000-0 +10174-2 0 00002
2 62854 53.1584 132.3290 0001322 76.5495 283.5655 15.34396754 08
| Epoch (UTC): | 25 May 2026 08:14:14 |
| Eccentricity: | 0.0001322 |
| inclination: | 53.1584° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 132.3290° |
| argument of perigee: | 76.5495° |
| revolutions per day: | 15.34396754 |
| mean anomaly at epoch: | 283.5655° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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