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 68878U 26145.58335647 +.00000000 +00000-0 -15199+0 0 00004
2 68878 51.8859 353.3663 0010599 236.2363 258.7360 15.09941553 06
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0010599 |
| inclination: | 51.8859° |
| perigee height: | 529 km |
| apogee height: | 544 km |
| right ascension of ascending node: | 353.3663° |
| argument of perigee: | 236.2363° |
| revolutions per day: | 15.09941553 |
| mean anomaly at epoch: | 258.7360° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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