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 44299U 26144.13934796 +.00000000 +00000-0 +00000-0 0 00000
2 44299 64.3666 193.4262 0012893 275.4828 134.9025 2.13102273 02
| Epoch (UTC): | 24 May 2026 03:20:39 |
| Eccentricity: | 0.0012893 |
| inclination: | 64.3666° |
| perigee height: | 19097 km |
| apogee height: | 19163 km |
| right ascension of ascending node: | 193.4262° |
| argument of perigee: | 275.4828° |
| revolutions per day: | 2.13102273 |
| mean anomaly at epoch: | 134.9025° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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