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 115U 60002D 23085.00209527 .00004737 00000-0 55898-3 0 9997
2 115 48.1640 85.9307 0033411 30.1192 330.1634 14.85791183363225
| Epoch (UTC): | 26 March 2023 00:03:01 |
| Eccentricity: | 0.0033411 |
| inclination: | 48.1640° |
| perigee height: | 588 km |
| apogee height: | 634 km |
| right ascension of ascending node: | 85.9307° |
| argument of perigee: | 30.1192° |
| revolutions per day: | 14.85791183 |
| mean anomaly at epoch: | 330.1634° |
| orbit number at epoch: | 36322 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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