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 26073.93813911 +.00000000 +00000-0 +64460-4 0 00006
2 25397 99.0030 64.3394 0002196 111.1627 248.9785 14.24407775 09
| Epoch (UTC): | 14 March 2026 22:30:55 |
| Eccentricity: | 0.0002196 |
| inclination: | 99.0030° |
| perigee height: | 809 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 64.3394° |
| argument of perigee: | 111.1627° |
| revolutions per day: | 14.24407775 |
| mean anomaly at epoch: | 248.9785° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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