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 68978U 26145.50003470 +.00000000 +00000-0 -28122-1 0 00005
2 68978 53.1591 268.2874 0001029 50.1165 35.3930 15.62352883 07
| Epoch (UTC): | 25 May 2026 12:00:02 |
| Eccentricity: | 0.0001029 |
| inclination: | 53.1591° |
| perigee height: | 380 km |
| apogee height: | 382 km |
| right ascension of ascending node: | 268.2874° |
| argument of perigee: | 50.1165° |
| revolutions per day: | 15.62352883 |
| mean anomaly at epoch: | 35.3930° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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