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 62992U 26145.02076280 +.00000000 +00000-0 +12220-2 0 00003
2 62992 43.0014 261.6845 0001674 37.4107 322.6877 15.70879169 02
| Epoch (UTC): | 25 May 2026 00:29:53 |
| Eccentricity: | 0.0001674 |
| inclination: | 43.0014° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 261.6845° |
| argument of perigee: | 37.4107° |
| revolutions per day: | 15.70879169 |
| mean anomaly at epoch: | 322.6877° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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