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 49393U 26145.40630170 +.00000000 +00000-0 +46161-3 0 00001
2 49393 35.0055 48.2172 0007428 177.8821 182.1926 15.23076975 01
| Epoch (UTC): | 25 May 2026 09:45:04 |
| Eccentricity: | 0.0007428 |
| inclination: | 35.0055° |
| perigee height: | 491 km |
| apogee height: | 502 km |
| right ascension of ascending node: | 48.2172° |
| argument of perigee: | 177.8821° |
| revolutions per day: | 15.23076975 |
| mean anomaly at epoch: | 182.1926° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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