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 is defined by the following mean orbital elements,
1 25634U 26017.19439105 +.00000000 +00000-0 +45266-4 0 00008
2 25634 98.4921 349.1326 0011141 115.0288 245.2047 14.19952967 03
| Epoch (UTC): | 17 January 2026 04:39:55 |
| Eccentricity: | 0.0011141 |
| inclination: | 98.4921° |
| perigee height: | 817 km |
| apogee height: | 834 km |
| right ascension of ascending node: | 349.1326° |
| argument of perigee: | 115.0288° |
| revolutions per day: | 14.19952967 |
| mean anomaly at epoch: | 245.2047° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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