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 60279U 26145.13800882 +.00000000 +00000-0 +11226-4 0 00001
2 60279 53.1620 57.4343 0001347 90.1201 269.9955 15.31698743 09
| Epoch (UTC): | 25 May 2026 03:18:43 |
| Eccentricity: | 0.0001347 |
| inclination: | 53.1620° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 57.4343° |
| argument of perigee: | 90.1201° |
| revolutions per day: | 15.31698743 |
| mean anomaly at epoch: | 269.9955° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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