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 04419U 26088.09651450 +.00000000 +00000-0 +70667-4 0 00005
2 04419 81.2164 314.7525 0038474 283.6116 76.0774 14.16161427 06
| Epoch (UTC): | 29 March 2026 02:18:58 |
| Eccentricity: | 0.0038474 |
| inclination: | 81.2164° |
| perigee height: | 811 km |
| apogee height: | 866 km |
| right ascension of ascending node: | 314.7525° |
| argument of perigee: | 283.6116° |
| revolutions per day: | 14.16161427 |
| mean anomaly at epoch: | 76.0774° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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