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 60998U 26145.03406833 +.00000000 +00000-0 +19790-4 0 00000
2 60998 53.1591 265.0375 0001261 323.6093 36.4839 15.69706157 02
| Epoch (UTC): | 25 May 2026 00:49:03 |
| Eccentricity: | 0.0001261 |
| inclination: | 53.1591° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 265.0375° |
| argument of perigee: | 323.6093° |
| revolutions per day: | 15.69706157 |
| mean anomaly at epoch: | 36.4839° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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