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 62881U 26145.16642757 +.00000000 +00000-0 +22423-2 0 00009
2 62881 43.0000 80.5491 0001198 282.3045 77.7689 15.70898237 08
| Epoch (UTC): | 25 May 2026 03:59:39 |
| Eccentricity: | 0.0001198 |
| inclination: | 43.0000° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 80.5491° |
| argument of perigee: | 282.3045° |
| revolutions per day: | 15.70898237 |
| mean anomaly at epoch: | 77.7689° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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