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 25400U 26021.44126881 +.00000000 +00000-0 +81721-4 0 00002
2 25400 98.8181 334.4929 0010362 146.2954 213.8886 14.26036510 09
| Epoch (UTC): | 21 January 2026 10:35:25 |
| Eccentricity: | 0.0010362 |
| inclination: | 98.8181° |
| perigee height: | 798 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 334.4929° |
| argument of perigee: | 146.2954° |
| revolutions per day: | 14.26036510 |
| mean anomaly at epoch: | 213.8886° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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