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 49205U 26145.50017676 +.00000000 +00000-0 +47164-3 0 00008
2 49205 87.8940 324.7468 0001513 88.5613 271.5689 13.13468725 01
| Epoch (UTC): | 25 May 2026 12:00:15 |
| Eccentricity: | 0.0001513 |
| inclination: | 87.8940° |
| perigee height: | 1209 km |
| apogee height: | 1211 km |
| right ascension of ascending node: | 324.7468° |
| argument of perigee: | 88.5613° |
| revolutions per day: | 13.13468725 |
| mean anomaly at epoch: | 271.5689° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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