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 25544U 26072.70791846 +.00000000 +00000-0 +22432-3 0 00008
2 25544 51.6324 52.4887 0007884 189.2977 170.7866 15.48633802 02
| Epoch (UTC): | 13 March 2026 16:59:24 |
| Eccentricity: | 0.0007884 |
| inclination: | 51.6324° |
| perigee height: | 415 km |
| apogee height: | 426 km |
| right ascension of ascending node: | 52.4887° |
| argument of perigee: | 189.2977° |
| revolutions per day: | 15.48633802 |
| mean anomaly at epoch: | 170.7866° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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