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 51974U 26145.42221953 +.00000000 +00000-0 +98805-4 0 00009
2 51974 53.1601 40.2994 0001070 121.0901 239.0205 15.30213537 05
| Epoch (UTC): | 25 May 2026 10:07:59 |
| Eccentricity: | 0.0001070 |
| inclination: | 53.1601° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 40.2994° |
| argument of perigee: | 121.0901° |
| revolutions per day: | 15.30213537 |
| mean anomaly at epoch: | 239.0205° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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