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 68183U 26145.35720227 +.00000000 +00000-0 +87077-3 0 00007
2 68183 53.1579 270.4735 0001330 69.7461 290.3687 15.38867195 04
| Epoch (UTC): | 25 May 2026 08:34:22 |
| Eccentricity: | 0.0001330 |
| inclination: | 53.1579° |
| perigee height: | 449 km |
| apogee height: | 450 km |
| right ascension of ascending node: | 270.4735° |
| argument of perigee: | 69.7461° |
| revolutions per day: | 15.38867195 |
| mean anomaly at epoch: | 290.3687° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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