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 02674U 67011A 23337.28152546 .00009428 00000-0 12451-2 0 9993
2 02674 39.9200 277.0226 0242624 37.1999 324.5322 14.61507881953872
| Epoch (UTC): | 03 December 2023 06:45:23 |
| Eccentricity: | 0.0242624 |
| inclination: | 39.9200° |
| perigee height: | 517 km |
| apogee height: | 860 km |
| right ascension of ascending node: | 277.0226° |
| argument of perigee: | 37.1999° |
| revolutions per day: | 14.61507881 |
| mean anomaly at epoch: | 324.5322° |
| orbit number at epoch: | 95387 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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