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 44481U 26145.60210109 +.00000000 +00000-0 +00000-0 0 00001
2 44481 1.4745 334.5400 0067754 1.6752 216.8174 1.00272597 05
| Epoch (UTC): | 25 May 2026 14:27:01 |
| Eccentricity: | 0.0067754 |
| inclination: | 1.4745° |
| perigee height: | 35501 km |
| apogee height: | 36072 km |
| right ascension of ascending node: | 334.5400° |
| argument of perigee: | 1.6752° |
| revolutions per day: | 1.00272597 |
| mean anomaly at epoch: | 216.8174° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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