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 60130U 26145.65849924 +.00000000 +00000-0 +25968-4 0 00002
2 60130 53.1609 28.9955 0001132 90.2253 269.8878 15.31698391 06
| Epoch (UTC): | 25 May 2026 15:48:14 |
| Eccentricity: | 0.0001132 |
| inclination: | 53.1609° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 28.9955° |
| argument of perigee: | 90.2253° |
| revolutions per day: | 15.31698391 |
| mean anomaly at epoch: | 269.8878° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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