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 49418U 26145.54304580 +.00000000 +00000-0 +70401-4 0 00002
2 49418 53.2151 244.1105 0001097 85.4202 274.6916 15.08840893 01
| Epoch (UTC): | 25 May 2026 13:01:59 |
| Eccentricity: | 0.0001097 |
| inclination: | 53.2151° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 244.1105° |
| argument of perigee: | 85.4202° |
| revolutions per day: | 15.08840893 |
| mean anomaly at epoch: | 274.6916° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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