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 26619U 00075A 23263.85572226 .00001431 00000-0 27094-3 0 9993
2 26619 97.9762 221.8389 0011091 61.4222 298.8096 14.65768375499868
| Epoch (UTC): | 20 September 2023 20:32:14 |
| Eccentricity: | 0.0011091 |
| inclination: | 97.9762° |
| perigee height: | 667 km |
| apogee height: | 682 km |
| right ascension of ascending node: | 221.8389° |
| argument of perigee: | 61.4222° |
| revolutions per day: | 14.65768375 |
| mean anomaly at epoch: | 298.8096° |
| orbit number at epoch: | 49986 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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