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 60257U 26145.17171941 +.00000000 +00000-0 +54507-4 0 00007
2 60257 53.1606 57.5155 0001209 78.1605 281.9531 15.30197940 08
| Epoch (UTC): | 25 May 2026 04:07:16 |
| Eccentricity: | 0.0001209 |
| inclination: | 53.1606° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 57.5155° |
| argument of perigee: | 78.1605° |
| revolutions per day: | 15.30197940 |
| mean anomaly at epoch: | 281.9531° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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