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 00059U 60013B 22027.48374607 .00000090 00000-0 -87783-6 0 9995
2 00059 28.2497 72.4552 0189071 190.0831 169.5885 13.52991681 26073
| Epoch (UTC): | 27 January 2022 11:36:35 |
| Eccentricity: | 0.0189071 |
| inclination: | 28.2497° |
| perigee height: | 920 km |
| apogee height: | 1202 km |
| right ascension of ascending node: | 72.4552° |
| argument of perigee: | 190.0831° |
| revolutions per day: | 13.52991681 |
| mean anomaly at epoch: | 169.5885° |
| orbit number at epoch: | 2607 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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