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 60947U 26145.62852288 +.00000000 +00000-0 +29611-3 0 00000
2 60947 34.9988 340.0014 0003650 192.4440 167.6185 15.23029987 09
| Epoch (UTC): | 25 May 2026 15:05:04 |
| Eccentricity: | 0.0003650 |
| inclination: | 34.9988° |
| perigee height: | 494 km |
| apogee height: | 499 km |
| right ascension of ascending node: | 340.0014° |
| argument of perigee: | 192.4440° |
| revolutions per day: | 15.23029987 |
| mean anomaly at epoch: | 167.6185° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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