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 30087U 99025QQ 24357.35004693 .00001658 00000-0 44452-3 0 9996
2 30087 98.4237 32.6614 0234000 101.4046 323.3338 14.34470282935984
| Epoch (UTC): | 22 December 2024 08:24:04 |
| Eccentricity: | 0.0234000 |
| inclination: | 98.4237° |
| perigee height: | 609 km |
| apogee height: | 944 km |
| right ascension of ascending node: | 32.6614° |
| argument of perigee: | 101.4046° |
| revolutions per day: | 14.34470282 |
| mean anomaly at epoch: | 323.3338° |
| orbit number at epoch: | 93598 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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