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 21878U 26087.98708684 +.00000000 +00000-0 +15396-2 0 00008
2 21878 90.1686 68.6547 0148857 46.5697 15.7405 13.51778937 07
| Epoch (UTC): | 28 March 2026 23:41:24 |
| Eccentricity: | 0.0148857 |
| inclination: | 90.1686° |
| perigee height: | 955 km |
| apogee height: | 1177 km |
| right ascension of ascending node: | 68.6547° |
| argument of perigee: | 46.5697° |
| revolutions per day: | 13.51778937 |
| mean anomaly at epoch: | 15.7405° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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