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 42829U 26153.02280562 +.00000000 +00000-0 +24723-3 0 00001
2 42829 97.4272 311.2609 0018927 141.2536 219.0052 15.04861453 05
| Epoch (UTC): | 02 June 2026 00:32:50 |
| Eccentricity: | 0.0018927 |
| inclination: | 97.4272° |
| perigee height: | 539 km |
| apogee height: | 565 km |
| right ascension of ascending node: | 311.2609° |
| argument of perigee: | 141.2536° |
| revolutions per day: | 15.04861453 |
| mean anomaly at epoch: | 219.0052° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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