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 37386U 11014A 23151.38469457 0.00000000 00000-0 00000-0 0 05
2 37386 63.4320 240.4497 0260681 357.2617 2.7383 13.40880262 08
| Epoch (UTC): | 31 May 2023 09:13:57 |
| Eccentricity: | 0.0260681 |
| inclination: | 63.4320° |
| perigee height: | 911 km |
| apogee height: | 1301 km |
| right ascension of ascending node: | 240.4497° |
| argument of perigee: | 357.2617° |
| revolutions per day: | 13.40880262 |
| mean anomaly at epoch: | 2.7383° |
| 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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