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 26150.48252141 +.00000000 +00000-0 +75918-3 0 00000
2 42827 97.4095 326.1305 0010069 133.8483 226.3589 15.25422948 02
| Epoch (UTC): | 30 May 2026 11:34:49 |
| Eccentricity: | 0.0010069 |
| inclination: | 97.4095° |
| perigee height: | 483 km |
| apogee height: | 496 km |
| right ascension of ascending node: | 326.1305° |
| argument of perigee: | 133.8483° |
| revolutions per day: | 15.25422948 |
| mean anomaly at epoch: | 226.3589° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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