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 62981U 26145.03653652 +.00000000 +00000-0 +12983-2 0 00002
2 62981 42.9992 260.9221 0001469 273.6417 86.4283 15.70891436 00
| Epoch (UTC): | 25 May 2026 00:52:36 |
| Eccentricity: | 0.0001469 |
| inclination: | 42.9992° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 260.9221° |
| argument of perigee: | 273.6417° |
| revolutions per day: | 15.70891436 |
| mean anomaly at epoch: | 86.4283° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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