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 60281U 26145.05155532 +.00000000 +00000-0 +34835-4 0 00001
2 60281 53.1608 57.6024 0001174 94.1211 265.9924 15.30193507 08
| Epoch (UTC): | 25 May 2026 01:14:14 |
| Eccentricity: | 0.0001174 |
| inclination: | 53.1608° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 57.6024° |
| argument of perigee: | 94.1211° |
| revolutions per day: | 15.30193507 |
| mean anomaly at epoch: | 265.9924° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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