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 49399U 26145.59061306 +.00000000 +00000-0 +22262-3 0 00002
2 49399 97.3341 181.6012 0015696 331.8668 28.1717 15.18065545 00
| Epoch (UTC): | 25 May 2026 14:10:28 |
| Eccentricity: | 0.0015696 |
| inclination: | 97.3341° |
| perigee height: | 501 km |
| apogee height: | 523 km |
| right ascension of ascending node: | 181.6012° |
| argument of perigee: | 331.8668° |
| revolutions per day: | 15.18065545 |
| mean anomaly at epoch: | 28.1717° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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