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 21419U 26088.00288978 +.00000000 +00000-0 +81109-4 0 00009
2 21419 74.0406 190.5265 0039333 53.7562 306.7215 14.35250534 03
| Epoch (UTC): | 29 March 2026 00:04:09 |
| Eccentricity: | 0.0039333 |
| inclination: | 74.0406° |
| perigee height: | 746 km |
| apogee height: | 802 km |
| right ascension of ascending node: | 190.5265° |
| argument of perigee: | 53.7562° |
| revolutions per day: | 14.35250534 |
| mean anomaly at epoch: | 306.7215° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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