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 42827U 26103.43087054 +.00000000 +00000-0 +34743-3 0 00003
2 42827 97.4084 279.5811 0008078 306.5840 53.4654 15.24297885 07
| Epoch (UTC): | 13 April 2026 10:20:27 |
| Eccentricity: | 0.0008078 |
| inclination: | 97.4084° |
| perigee height: | 487 km |
| apogee height: | 498 km |
| right ascension of ascending node: | 279.5811° |
| argument of perigee: | 306.5840° |
| revolutions per day: | 15.24297885 |
| mean anomaly at epoch: | 53.4654° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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