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 49005U 21061C 23268.08105324 .00011961 00000-0 61614-3 0 9991
2 49005 97.4374 329.2729 0007444 63.6892 296.5105 15.16516704122998
| Epoch (UTC): | 25 September 2023 01:56:43 |
| Eccentricity: | 0.0007444 |
| inclination: | 97.4374° |
| perigee height: | 511 km |
| apogee height: | 521 km |
| right ascension of ascending node: | 329.2729° |
| argument of perigee: | 63.6892° |
| revolutions per day: | 15.16516704 |
| mean anomaly at epoch: | 296.5105° |
| orbit number at epoch: | 12299 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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