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 26496U 00054C 24279.11120912 .00000074 00000-0 10981-2 0 9999
2 26496 7.2321 85.8273 7179054 195.9859 116.4898 2.24195697197072
| Epoch (UTC): | 05 October 2024 02:40:08 |
| Eccentricity: | 0.7179054 |
| inclination: | 7.2321° |
| perigee height: | 578 km |
| apogee height: | 35984 km |
| right ascension of ascending node: | 85.8273° |
| argument of perigee: | 195.9859° |
| revolutions per day: | 2.24195697 |
| mean anomaly at epoch: | 116.4898° |
| orbit number at epoch: | 19707 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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