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 data is extracted from the following two-line orbital elements,
1 04211U 69082CA 24357.80140984 .00000817 00000-0 48183-3 0 9991
2 04211 70.0725 141.1872 0033481 347.5238 12.5044 14.11070442836643
| Epoch (UTC): | 22 December 2024 19:14:01 |
| Eccentricity: | 0.0033481 |
| inclination: | 70.0725° |
| perigee height: | 831 km |
| apogee height: | 880 km |
| right ascension of ascending node: | 141.1872° |
| argument of perigee: | 347.5238° |
| revolutions per day: | 14.11070442 |
| mean anomaly at epoch: | 12.5044° |
| orbit number at epoch: | 83664 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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