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 26106.18582810 +.00000000 +00000-0 +12651-3 0 00006
2 42849 97.4197 274.1184 0009816 322.5132 37.5411 15.07332483 02
| Epoch (UTC): | 16 April 2026 04:27:35 |
| Eccentricity: | 0.0009816 |
| inclination: | 97.4197° |
| perigee height: | 538 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 274.1184° |
| argument of perigee: | 322.5132° |
| revolutions per day: | 15.07332483 |
| mean anomaly at epoch: | 37.5411° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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