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 00115U 60002D 22274.87571188 .00002578 00000-0 32459-3 0 9995
2 00115 48.1667 210.0938 0034371 336.3774 23.5560 14.84670666316037
| Epoch (UTC): | 01 October 2022 21:01:01 |
| Eccentricity: | 0.0034371 |
| inclination: | 48.1667° |
| perigee height: | 590 km |
| apogee height: | 638 km |
| right ascension of ascending node: | 210.0938° |
| argument of perigee: | 336.3774° |
| revolutions per day: | 14.84670666 |
| mean anomaly at epoch: | 23.5560° |
| orbit number at epoch: | 31603 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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