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 25544U 98067A 25342.54239145 .00012445 00000-0 23028-3 0 9993
2 25544 51.6307 163.2617 0003394 220.7658 139.3077 15.49420853542203
| Epoch (UTC): | 08 December 2025 13:01:02 |
| Eccentricity: | 0.0003394 |
| inclination: | 51.6307° |
| perigee height: | 416 km |
| apogee height: | 421 km |
| right ascension of ascending node: | 163.2617° |
| argument of perigee: | 220.7658° |
| revolutions per day: | 15.49420853 |
| mean anomaly at epoch: | 139.3077° |
| orbit number at epoch: | 54220 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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