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 49437U 26145.60010444 +.00000000 +00000-0 +62334-4 0 00009
2 49437 53.2123 223.8555 0001138 92.3937 267.7185 15.08837088 05
| Epoch (UTC): | 25 May 2026 14:24:09 |
| Eccentricity: | 0.0001138 |
| inclination: | 53.2123° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 223.8555° |
| argument of perigee: | 92.3937° |
| revolutions per day: | 15.08837088 |
| mean anomaly at epoch: | 267.7185° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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