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 60012U 26145.50854108 +.00000000 +00000-0 +32835-3 0 00005
2 60012 97.5683 237.3543 0007868 344.0553 16.0429 15.12967315 01
| Epoch (UTC): | 25 May 2026 12:12:17 |
| Eccentricity: | 0.0007868 |
| inclination: | 97.5683° |
| perigee height: | 522 km |
| apogee height: | 533 km |
| right ascension of ascending node: | 237.3543° |
| argument of perigee: | 344.0553° |
| revolutions per day: | 15.12967315 |
| mean anomaly at epoch: | 16.0429° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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