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 40012U 14033C 25190.45895140 .00002123 00000-0 24768-3 0 9999
2 40012 97.7448 345.8237 0048977 116.1210 244.5056 14.85375018595239
| Epoch (UTC): | 09 July 2025 11:00:53 |
| Eccentricity: | 0.0048977 |
| inclination: | 97.7448° |
| perigee height: | 578 km |
| apogee height: | 646 km |
| right ascension of ascending node: | 345.8237° |
| argument of perigee: | 116.1210° |
| revolutions per day: | 14.85375018 |
| mean anomaly at epoch: | 244.5056° |
| orbit number at epoch: | 59523 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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