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 51970U 26145.43488380 +.00000000 +00000-0 +22817-4 0 00005
2 51970 53.1607 40.2409 0001134 90.4769 269.6361 15.30190878 04
| Epoch (UTC): | 25 May 2026 10:26:13 |
| Eccentricity: | 0.0001134 |
| inclination: | 53.1607° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 40.2409° |
| argument of perigee: | 90.4769° |
| revolutions per day: | 15.30190878 |
| mean anomaly at epoch: | 269.6361° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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