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 01521U 26088.11548520 +.00000000 +00000-0 +34454-4 0 00006
2 01521 90.0204 210.1189 0071078 126.9778 46.1102 13.33280718 01
| Epoch (UTC): | 29 March 2026 02:46:17 |
| Eccentricity: | 0.0071078 |
| inclination: | 90.0204° |
| perigee height: | 1081 km |
| apogee height: | 1188 km |
| right ascension of ascending node: | 210.1189° |
| argument of perigee: | 126.9778° |
| revolutions per day: | 13.33280718 |
| mean anomaly at epoch: | 46.1102° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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