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 63070U 26145.50885588 +.00000000 +00000-0 +75442-3 0 00009
2 63070 43.0053 73.6525 0001617 274.7348 85.3319 15.27595623 05
| Epoch (UTC): | 25 May 2026 12:12:45 |
| Eccentricity: | 0.0001617 |
| inclination: | 43.0053° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 73.6525° |
| argument of perigee: | 274.7348° |
| revolutions per day: | 15.27595623 |
| mean anomaly at epoch: | 85.3319° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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