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 42846U 26150.39092146 +.00000000 +00000-0 +36930-3 0 00009
2 42846 97.4049 312.4361 0013432 167.0221 193.1354 15.06170101 09
| Epoch (UTC): | 30 May 2026 09:22:55 |
| Eccentricity: | 0.0013432 |
| inclination: | 97.4049° |
| perigee height: | 539 km |
| apogee height: | 557 km |
| right ascension of ascending node: | 312.4361° |
| argument of perigee: | 167.0221° |
| revolutions per day: | 15.06170101 |
| mean anomaly at epoch: | 193.1354° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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