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 45399U 26145.25222137 +.00000000 +00000-0 +99530-3 0 00004
2 45399 53.0347 90.4888 0006027 69.1109 291.0549 15.64121165 04
| Epoch (UTC): | 25 May 2026 06:03:11 |
| Eccentricity: | 0.0006027 |
| inclination: | 53.0347° |
| perigee height: | 372 km |
| apogee height: | 380 km |
| right ascension of ascending node: | 90.4888° |
| argument of perigee: | 69.1109° |
| revolutions per day: | 15.64121165 |
| mean anomaly at epoch: | 291.0549° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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