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 23097U 94026A 23249.79451539 -.00000093 00000-0 00000-0 0 01
2 23097 62.6968 245.9860 6744890 263.1339 21.9068 2.00599001 01
| Epoch (UTC): | 06 September 2023 19:04:06 |
| Eccentricity: | 0.6744890 |
| inclination: | 62.6968° |
| perigee height: | 2266 km |
| apogee height: | 38091 km |
| right ascension of ascending node: | 245.9860° |
| argument of perigee: | 263.1339° |
| revolutions per day: | 2.00599001 |
| mean anomaly at epoch: | 21.9068° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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