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 60016U 26145.50700543 +.00000000 +00000-0 +37298-5 0 00002
2 60016 53.1609 78.8877 0001096 84.5036 275.6090 15.31704534 08
| Epoch (UTC): | 25 May 2026 12:10:05 |
| Eccentricity: | 0.0001096 |
| inclination: | 53.1609° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 78.8877° |
| argument of perigee: | 84.5036° |
| revolutions per day: | 15.31704534 |
| mean anomaly at epoch: | 275.6090° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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