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 44978U 26145.53377181 +.00000000 +00000-0 +00000-0 0 00008
2 44978 0.0647 275.3747 0007045 125.5246 141.9047 1.00270472 06
| Epoch (UTC): | 25 May 2026 12:48:37 |
| Eccentricity: | 0.0007045 |
| inclination: | 0.0647° |
| perigee height: | 35757 km |
| apogee height: | 35817 km |
| right ascension of ascending node: | 275.3747° |
| argument of perigee: | 125.5246° |
| revolutions per day: | 1.00270472 |
| mean anomaly at epoch: | 141.9047° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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