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 48274U 21035A 22274.44304861 .00008732 00000-0 10300-3 0 9990
2 48274 41.4721 291.4733 0002902 308.0624 195.7218 15.61467698 81387
| Epoch (UTC): | 01 October 2022 10:37:59 |
| Eccentricity: | 0.0002902 |
| inclination: | 41.4721° |
| perigee height: | 381 km |
| apogee height: | 385 km |
| right ascension of ascending node: | 291.4733° |
| argument of perigee: | 308.0624° |
| revolutions per day: | 15.61467698 |
| mean anomaly at epoch: | 195.7218° |
| orbit number at epoch: | 8138 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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