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 26725U 01012B 23267.04080310 -.00000264 00000-0 -55092-2 0 9999
2 26725 1.3615 357.3743 7052949 158.7025 204.4216 2.23578542183982
| Epoch (UTC): | 24 September 2023 00:58:45 |
| Eccentricity: | 0.7052949 |
| inclination: | 1.3615° |
| perigee height: | 902 km |
| apogee height: | 35750 km |
| right ascension of ascending node: | 357.3743° |
| argument of perigee: | 158.7025° |
| revolutions per day: | 2.23578542 |
| mean anomaly at epoch: | 204.4216° |
| orbit number at epoch: | 18398 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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