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 49408U 26145.50003470 +.00000000 +00000-0 +14672-2 0 00007
2 49408 53.2137 214.7164 0001998 61.5947 287.1641 15.84993788 03
| Epoch (UTC): | 25 May 2026 12:00:02 |
| Eccentricity: | 0.0001998 |
| inclination: | 53.2137° |
| perigee height: | 315 km |
| apogee height: | 318 km |
| right ascension of ascending node: | 214.7164° |
| argument of perigee: | 61.5947° |
| revolutions per day: | 15.84993788 |
| mean anomaly at epoch: | 287.1641° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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