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 28415U 04035C 23151.67842526 .00002962 00000-0 17772-3 0 9990
2 28415 97.4698 189.1790 0045507 264.6456 94.9581 15.10854777 26126
| Epoch (UTC): | 31 May 2023 16:16:55 |
| Eccentricity: | 0.0045507 |
| inclination: | 97.4698° |
| perigee height: | 502 km |
| apogee height: | 565 km |
| right ascension of ascending node: | 189.1790° |
| argument of perigee: | 264.6456° |
| revolutions per day: | 15.10854777 |
| mean anomaly at epoch: | 94.9581° |
| orbit number at epoch: | 2612 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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