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 61218U 26145.46901470 +.00000000 +00000-0 +14691-4 0 00005
2 61218 53.1606 325.8182 0001183 96.2887 263.8249 15.30195705 03
| Epoch (UTC): | 25 May 2026 11:15:22 |
| Eccentricity: | 0.0001183 |
| inclination: | 53.1606° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 325.8182° |
| argument of perigee: | 96.2887° |
| revolutions per day: | 15.30195705 |
| mean anomaly at epoch: | 263.8249° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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