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 25756U 99029A 23082.90057028 .00000865 00000-0 21562-3 0 9998
2 25756 98.6189 62.2002 0012387 272.3172 87.6605 14.54220245263243
| Epoch (UTC): | 23 March 2023 21:36:49 |
| Eccentricity: | 0.0012387 |
| inclination: | 98.6189° |
| perigee height: | 703 km |
| apogee height: | 720 km |
| right ascension of ascending node: | 62.2002° |
| argument of perigee: | 272.3172° |
| revolutions per day: | 14.54220245 |
| mean anomaly at epoch: | 87.6605° |
| orbit number at epoch: | 26324 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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