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 63052U 26145.05553883 +.00000000 +00000-0 +12540-2 0 00008
2 63052 43.0000 274.8195 0001587 40.5277 319.5708 15.70879999 04
| Epoch (UTC): | 25 May 2026 01:19:58 |
| Eccentricity: | 0.0001587 |
| inclination: | 43.0000° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 274.8195° |
| argument of perigee: | 40.5277° |
| revolutions per day: | 15.70879999 |
| mean anomaly at epoch: | 319.5708° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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