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 42849U 26162.93748360 +.00000000 +00000-0 +24706-3 0 00009
2 42849 97.4244 328.8844 0012234 118.2738 241.9726 15.07721757 01
| Epoch (UTC): | 11 June 2026 22:29:58 |
| Eccentricity: | 0.0012234 |
| inclination: | 97.4244° |
| perigee height: | 535 km |
| apogee height: | 552 km |
| right ascension of ascending node: | 328.8844° |
| argument of perigee: | 118.2738° |
| revolutions per day: | 15.07721757 |
| mean anomaly at epoch: | 241.9726° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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