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 68941U 26145.38891551 +.00000000 +00000-0 +42695-3 0 00008
2 68941 51.8750 177.7105 0006827 71.7351 288.4376 15.33693690 04
| Epoch (UTC): | 25 May 2026 09:20:02 |
| Eccentricity: | 0.0006827 |
| inclination: | 51.8750° |
| perigee height: | 460 km |
| apogee height: | 469 km |
| right ascension of ascending node: | 177.7105° |
| argument of perigee: | 71.7351° |
| revolutions per day: | 15.33693690 |
| mean anomaly at epoch: | 288.4376° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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