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 25399U 26105.94986593 +.00000000 +00000-0 +37573-4 0 00007
2 25399 98.9743 91.5486 0000944 322.2237 37.8876 14.25603916 07
| Epoch (UTC): | 15 April 2026 22:47:48 |
| Eccentricity: | 0.0000944 |
| inclination: | 98.9743° |
| perigee height: | 806 km |
| apogee height: | 807 km |
| right ascension of ascending node: | 91.5486° |
| argument of perigee: | 322.2237° |
| revolutions per day: | 14.25603916 |
| mean anomaly at epoch: | 37.8876° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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