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 44881U 19093C 23332.55108012 .00002184 00000-0 27478-3 0 9998
2 44881 97.8498 48.1382 0013202 261.0377 98.9343 14.83024465213157
| Epoch (UTC): | 28 November 2023 13:13:33 |
| Eccentricity: | 0.0013202 |
| inclination: | 97.8498° |
| perigee height: | 610 km |
| apogee height: | 629 km |
| right ascension of ascending node: | 48.1382° |
| argument of perigee: | 261.0377° |
| revolutions per day: | 14.83024465 |
| mean anomaly at epoch: | 98.9343° |
| orbit number at epoch: | 21315 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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