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 68877U 26144.99505072 +.00000000 +00000-0 +95538-3 0 00006
2 68877 51.8857 354.3551 0002293 182.4525 177.6452 15.38625043 00
| Epoch (UTC): | 24 May 2026 23:52:52 |
| Eccentricity: | 0.0002293 |
| inclination: | 51.8857° |
| perigee height: | 449 km |
| apogee height: | 452 km |
| right ascension of ascending node: | 354.3551° |
| argument of perigee: | 182.4525° |
| revolutions per day: | 15.38625043 |
| mean anomaly at epoch: | 177.6452° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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