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 51948U 26145.64017418 +.00000000 +00000-0 +63279-3 0 00009
2 51948 63.4953 347.7516 0100764 350.1257 9.7873 15.18024262 08
| Epoch (UTC): | 25 May 2026 15:21:51 |
| Eccentricity: | 0.0100764 |
| inclination: | 63.4953° |
| perigee height: | 442 km |
| apogee height: | 581 km |
| right ascension of ascending node: | 347.7516° |
| argument of perigee: | 350.1257° |
| revolutions per day: | 15.18024262 |
| mean anomaly at epoch: | 9.7873° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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