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 23080.42909417 .00003571 00000-0 42829-3 0 9998
2 00115 48.1637 107.9979 0033656 9.7284 350.4274 14.85746852341387
| Epoch (UTC): | 21 March 2023 10:17:53 |
| Eccentricity: | 0.0033656 |
| inclination: | 48.1637° |
| perigee height: | 588 km |
| apogee height: | 635 km |
| right ascension of ascending node: | 107.9979° |
| argument of perigee: | 9.7284° |
| revolutions per day: | 14.85746852 |
| mean anomaly at epoch: | 350.4274° |
| orbit number at epoch: | 34138 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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