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 60994U 26145.30346852 +.00000000 +00000-0 +24471-4 0 00002
2 60994 53.1596 263.8859 0001032 77.0126 283.1007 15.69703146 02
| Epoch (UTC): | 25 May 2026 07:16:59 |
| Eccentricity: | 0.0001032 |
| inclination: | 53.1596° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 263.8859° |
| argument of perigee: | 77.0126° |
| revolutions per day: | 15.69703146 |
| mean anomaly at epoch: | 283.1007° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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