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 26150.46005209 +.00000000 +00000-0 +32217-3 0 00008
2 42849 97.4235 316.8384 0011597 156.5029 203.6731 15.07623049 02
| Epoch (UTC): | 30 May 2026 11:02:28 |
| Eccentricity: | 0.0011597 |
| inclination: | 97.4235° |
| perigee height: | 535 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 316.8384° |
| argument of perigee: | 156.5029° |
| revolutions per day: | 15.07623049 |
| mean anomaly at epoch: | 203.6731° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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