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 30349U 99025ABL 25195.63812855 .00002523 00000-0 14013-2 0 9997
2 30349 98.5699 164.9663 0091455 81.8181 333.0864 14.09859190941011
| Epoch (UTC): | 14 July 2025 15:18:54 |
| Eccentricity: | 0.0091455 |
| inclination: | 98.5699° |
| perigee height: | 793 km |
| apogee height: | 926 km |
| right ascension of ascending node: | 164.9663° |
| argument of perigee: | 81.8181° |
| revolutions per day: | 14.09859190 |
| mean anomaly at epoch: | 333.0864° |
| orbit number at epoch: | 94101 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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