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 40014U 14033E 25167.16639594 .00002890 00000-0 17593-3 0 9991
2 40014 98.0733 234.1107 0030478 349.3870 10.6712 15.10928970600493
| Epoch (UTC): | 16 June 2025 03:59:36 |
| Eccentricity: | 0.0030478 |
| inclination: | 98.0733° |
| perigee height: | 512 km |
| apogee height: | 554 km |
| right ascension of ascending node: | 234.1107° |
| argument of perigee: | 349.3870° |
| revolutions per day: | 15.10928970 |
| mean anomaly at epoch: | 10.6712° |
| orbit number at epoch: | 60049 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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