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 49281U 26145.42517912 +.00000000 +00000-0 +11263-3 0 00002
2 49281 87.9176 278.9794 0001869 99.9658 260.1687 13.20769731 09
| Epoch (UTC): | 25 May 2026 10:12:15 |
| Eccentricity: | 0.0001869 |
| inclination: | 87.9176° |
| perigee height: | 1180 km |
| apogee height: | 1183 km |
| right ascension of ascending node: | 278.9794° |
| argument of perigee: | 99.9658° |
| revolutions per day: | 13.20769731 |
| mean anomaly at epoch: | 260.1687° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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