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 49075U 26145.34159450 +.00000000 +00000-0 +12291-2 0 00004
2 49075 87.8959 355.2052 0001719 85.6424 274.4901 13.12441354 07
| Epoch (UTC): | 25 May 2026 08:11:53 |
| Eccentricity: | 0.0001719 |
| inclination: | 87.8959° |
| perigee height: | 1212 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 355.2052° |
| argument of perigee: | 85.6424° |
| revolutions per day: | 13.12441354 |
| mean anomaly at epoch: | 274.4901° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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