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 42840U 26144.92602269 +.00000000 +00000-0 +53815-3 0 00009
2 42840 97.3771 323.6829 0008566 140.5686 219.6180 15.29353072 06
| Epoch (UTC): | 24 May 2026 22:13:28 |
| Eccentricity: | 0.0008566 |
| inclination: | 97.3771° |
| perigee height: | 472 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 323.6829° |
| argument of perigee: | 140.5686° |
| revolutions per day: | 15.29353072 |
| mean anomaly at epoch: | 219.6180° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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