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 60291U 26145.16951135 +.00000000 +00000-0 +47381-4 0 00007
2 60291 53.1610 56.9166 0001216 86.1878 273.9261 15.30204507 04
| Epoch (UTC): | 25 May 2026 04:04:05 |
| Eccentricity: | 0.0001216 |
| inclination: | 53.1610° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 56.9166° |
| argument of perigee: | 86.1878° |
| revolutions per day: | 15.30204507 |
| mean anomaly at epoch: | 273.9261° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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