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 40912U 15049P 22181.11744259 .00007925 00000-0 30751-3 0 9994
2 40912 97.4356 192.4585 0010773 256.0606 177.2505 15.26327462375683
| Epoch (UTC): | 30 June 2022 02:49:07 |
| Eccentricity: | 0.0010773 |
| inclination: | 97.4356° |
| perigee height: | 479 km |
| apogee height: | 494 km |
| right ascension of ascending node: | 192.4585° |
| argument of perigee: | 256.0606° |
| revolutions per day: | 15.26327462 |
| mean anomaly at epoch: | 177.2505° |
| orbit number at epoch: | 37568 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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