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 26050.40048444 +.00000000 +00000-0 +34181-3 0 00009
2 42829 97.4103 212.7038 0018628 134.6673 225.6075 15.04096527 05
| Epoch (UTC): | 19 February 2026 09:36:41 |
| Eccentricity: | 0.0018628 |
| inclination: | 97.4103° |
| perigee height: | 541 km |
| apogee height: | 567 km |
| right ascension of ascending node: | 212.7038° |
| argument of perigee: | 134.6673° |
| revolutions per day: | 15.04096527 |
| mean anomaly at epoch: | 225.6075° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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