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 62304U 26145.50603102 +.00000000 +00000-0 +42440-3 0 00000
2 62304 53.1586 184.4215 0001040 72.2934 287.8180 15.30203175 03
| Epoch (UTC): | 25 May 2026 12:08:41 |
| Eccentricity: | 0.0001040 |
| inclination: | 53.1586° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 184.4215° |
| argument of perigee: | 72.2934° |
| revolutions per day: | 15.30203175 |
| mean anomaly at epoch: | 287.8180° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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