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 28874U 26145.41016624 +.00000000 +00000-0 +00000-0 0 00004
2 28874 54.8973 274.0963 0127735 296.0095 59.1466 2.00567255 07
| Epoch (UTC): | 25 May 2026 09:50:38 |
| Eccentricity: | 0.0127735 |
| inclination: | 54.8973° |
| perigee height: | 19843 km |
| apogee height: | 20521 km |
| right ascension of ascending node: | 274.0963° |
| argument of perigee: | 296.0095° |
| revolutions per day: | 2.00567255 |
| mean anomaly at epoch: | 59.1466° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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