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 60418U 26145.54311503 +.00000000 +00000-0 +44730-4 0 00004
2 60418 53.1610 245.1537 0001232 80.4338 279.6804 15.34390456 04
| Epoch (UTC): | 25 May 2026 13:02:05 |
| Eccentricity: | 0.0001232 |
| inclination: | 53.1610° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 245.1537° |
| argument of perigee: | 80.4338° |
| revolutions per day: | 15.34390456 |
| mean anomaly at epoch: | 279.6804° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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