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 26702U 01007A 24358.08907383 .00024566 00000-0 80923-3 0 9993
2 26702 97.4655 13.4687 0006208 349.5943 10.5168 15.31451873306331
| Epoch (UTC): | 23 December 2024 02:08:15 |
| Eccentricity: | 0.0006208 |
| inclination: | 97.4655° |
| perigee height: | 467 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 13.4687° |
| argument of perigee: | 349.5943° |
| revolutions per day: | 15.31451873 |
| mean anomaly at epoch: | 10.5168° |
| orbit number at epoch: | 30633 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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