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 23088.29726688 .00004342 00000-0 51430-3 0 9993
2 00115 48.1649 70.0303 0033353 44.8869 315.4734 14.85816636342554
| Epoch (UTC): | 29 March 2023 07:08:03 |
| Eccentricity: | 0.0033353 |
| inclination: | 48.1649° |
| perigee height: | 588 km |
| apogee height: | 634 km |
| right ascension of ascending node: | 70.0303° |
| argument of perigee: | 44.8869° |
| revolutions per day: | 14.85816636 |
| mean anomaly at epoch: | 315.4734° |
| orbit number at epoch: | 34255 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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