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 42104U 26095.34418354 +.00000000 +00000-0 +44806-3 0 00003
2 42104 82.8745 127.2732 0039703 247.0476 112.6492 13.81926399 09
| Epoch (UTC): | 05 April 2026 08:15:37 |
| Eccentricity: | 0.0039703 |
| inclination: | 82.8745° |
| perigee height: | 928 km |
| apogee height: | 986 km |
| right ascension of ascending node: | 127.2732° |
| argument of perigee: | 247.0476° |
| revolutions per day: | 13.81926399 |
| mean anomaly at epoch: | 112.6492° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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