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 15360U 26066.83467233 +.00000000 +00000-0 +14247-3 0 00005
2 15360 82.9414 200.8198 0042248 139.7625 220.6673 13.77055453 02
| Epoch (UTC): | 07 March 2026 20:01:55 |
| Eccentricity: | 0.0042248 |
| inclination: | 82.9414° |
| perigee height: | 943 km |
| apogee height: | 1005 km |
| right ascension of ascending node: | 200.8198° |
| argument of perigee: | 139.7625° |
| revolutions per day: | 13.77055453 |
| mean anomaly at epoch: | 220.6673° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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