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 33498U 09002G 23340.30573422 .00003683 00000-0 45465-3 0 9993
2 33498 98.1250 245.9619 0009347 325.4494 34.6111 14.83455166800911
| Epoch (UTC): | 06 December 2023 07:20:15 |
| Eccentricity: | 0.0009347 |
| inclination: | 98.1250° |
| perigee height: | 612 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 245.9619° |
| argument of perigee: | 325.4494° |
| revolutions per day: | 14.83455166 |
| mean anomaly at epoch: | 34.6111° |
| orbit number at epoch: | 80091 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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