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 60999U 26145.34751601 +.00000000 +00000-0 +14276-2 0 00003
2 60999 53.1561 263.4395 0001117 69.0206 291.0931 15.69771716 06
| Epoch (UTC): | 25 May 2026 08:20:25 |
| Eccentricity: | 0.0001117 |
| inclination: | 53.1561° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 263.4395° |
| argument of perigee: | 69.0206° |
| revolutions per day: | 15.69771716 |
| mean anomaly at epoch: | 291.0931° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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