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 60081U 26145.58122457 +.00000000 +00000-0 +10112-3 0 00008
2 60081 97.9854 169.7191 0000637 113.1322 246.9957 14.80583467 00
| Epoch (UTC): | 25 May 2026 13:56:57 |
| Eccentricity: | 0.0000637 |
| inclination: | 97.9854° |
| perigee height: | 627 km |
| apogee height: | 628 km |
| right ascension of ascending node: | 169.7191° |
| argument of perigee: | 113.1322° |
| revolutions per day: | 14.80583467 |
| mean anomaly at epoch: | 246.9957° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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