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 16719U 86034A 25197.08150920 .00014398 00000-0 31557-3 0 9993
2 16719 82.5408 318.9056 0007391 74.5094 285.6970 15.43921799143896
| Epoch (UTC): | 16 July 2025 01:57:22 |
| Eccentricity: | 0.0007391 |
| inclination: | 82.5408° |
| perigee height: | 429 km |
| apogee height: | 439 km |
| right ascension of ascending node: | 318.9056° |
| argument of perigee: | 74.5094° |
| revolutions per day: | 15.43921799 |
| mean anomaly at epoch: | 285.6970° |
| orbit number at epoch: | 14389 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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