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 25338U 98030A 25194.18744568 .00000181 00000-0 91874-4 0 9998
2 25338 98.5338 218.5076 0009020 259.5880 100.4284 14.26995837413197
| Epoch (UTC): | 13 July 2025 04:29:55 |
| Eccentricity: | 0.0009020 |
| inclination: | 98.5338° |
| perigee height: | 795 km |
| apogee height: | 808 km |
| right ascension of ascending node: | 218.5076° |
| argument of perigee: | 259.5880° |
| revolutions per day: | 14.26995837 |
| mean anomaly at epoch: | 100.4284° |
| orbit number at epoch: | 41319 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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