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 45465U 26145.61091948 +.00000000 +00000-0 +00000-0 0 00003
2 45465 2.5974 300.8920 0044490 18.0860 281.9244 1.00269492 02
| Epoch (UTC): | 25 May 2026 14:39:43 |
| Eccentricity: | 0.0044490 |
| inclination: | 2.5974° |
| perigee height: | 35600 km |
| apogee height: | 35975 km |
| right ascension of ascending node: | 300.8920° |
| argument of perigee: | 18.0860° |
| revolutions per day: | 1.00269492 |
| mean anomaly at epoch: | 281.9244° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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