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 23152.34072077 .00003400 00000-0 20338-3 0 9991
2 28415 97.4696 189.8257 0045543 262.2567 97.3491 15.10859662 26222
| Epoch (UTC): | 01 June 2023 08:10:38 |
| Eccentricity: | 0.0045543 |
| inclination: | 97.4696° |
| perigee height: | 502 km |
| apogee height: | 565 km |
| right ascension of ascending node: | 189.8257° |
| argument of perigee: | 262.2567° |
| revolutions per day: | 15.10859662 |
| mean anomaly at epoch: | 97.3491° |
| orbit number at epoch: | 2622 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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