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 21610U 26088.16495676 +.00000000 +00000-0 +12156-3 0 00009
2 21610 98.1971 139.6668 0003519 36.7160 323.4271 14.42907726 01
| Epoch (UTC): | 29 March 2026 03:57:32 |
| Eccentricity: | 0.0003519 |
| inclination: | 98.1971° |
| perigee height: | 746 km |
| apogee height: | 751 km |
| right ascension of ascending node: | 139.6668° |
| argument of perigee: | 36.7160° |
| revolutions per day: | 14.42907726 |
| mean anomaly at epoch: | 323.4271° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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