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 60233U 26145.59204846 +.00000000 +00000-0 +00000-0 0 00003
2 60233 0.0188 181.9965 0001381 303.5007 12.8257 1.00272720 09
| Epoch (UTC): | 25 May 2026 14:12:32 |
| Eccentricity: | 0.0001381 |
| inclination: | 0.0188° |
| perigee height: | 35781 km |
| apogee height: | 35792 km |
| right ascension of ascending node: | 181.9965° |
| argument of perigee: | 303.5007° |
| revolutions per day: | 1.00272720 |
| mean anomaly at epoch: | 12.8257° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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