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 23037.04573732 .00002534 00000-0 31485-3 0 9999
2 115 48.1666 317.2478 0033643 179.4554 180.6402 14.85292975356092
| Epoch (UTC): | 06 February 2023 01:05:51 |
| Eccentricity: | 0.0033643 |
| inclination: | 48.1666° |
| perigee height: | 589 km |
| apogee height: | 636 km |
| right ascension of ascending node: | 317.2478° |
| argument of perigee: | 179.4554° |
| revolutions per day: | 14.85292975 |
| mean anomaly at epoch: | 180.6402° |
| orbit number at epoch: | 35609 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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