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 35296U 97051PL 23265.43941087 .00013940 00000-0 25739-2 0 9996
2 35296 86.3099 319.3500 0004456 245.0259 115.0491 14.65369284592532
| Epoch (UTC): | 22 September 2023 10:32:45 |
| Eccentricity: | 0.0004456 |
| inclination: | 86.3099° |
| perigee height: | 673 km |
| apogee height: | 679 km |
| right ascension of ascending node: | 319.3500° |
| argument of perigee: | 245.0259° |
| revolutions per day: | 14.65369284 |
| mean anomaly at epoch: | 115.0491° |
| orbit number at epoch: | 59253 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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