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 25397U 26074.92155531 +.00000000 +00000-0 +52883-4 0 00009
2 25397 99.0032 65.3470 0002216 109.3629 250.7789 14.24407912 09
| Epoch (UTC): | 15 March 2026 22:07:02 |
| Eccentricity: | 0.0002216 |
| inclination: | 99.0032° |
| perigee height: | 809 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 65.3470° |
| argument of perigee: | 109.3629° |
| revolutions per day: | 14.24407912 |
| mean anomaly at epoch: | 250.7789° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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