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 40964U 15058A 23078.20122965 0.00000000 00000-0 00000-0 0 02
2 40964 63.4360 214.4715 0110695 1.5136 358.4864 13.40861842 04
| Epoch (UTC): | 19 March 2023 04:49:46 |
| Eccentricity: | 0.0110695 |
| inclination: | 63.4360° |
| perigee height: | 1023 km |
| apogee height: | 1189 km |
| right ascension of ascending node: | 214.4715° |
| argument of perigee: | 1.5136° |
| revolutions per day: | 13.40861842 |
| mean anomaly at epoch: | 358.4864° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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