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 00029U 26160.02473808 +.00000000 +00000-0 +87798-4 0 00004
2 00029 48.3789 63.4378 0022501 234.5428 125.3385 14.78765427 09
| Epoch (UTC): | 09 June 2026 00:35:37 |
| Eccentricity: | 0.0022501 |
| inclination: | 48.3789° |
| perigee height: | 617 km |
| apogee height: | 649 km |
| right ascension of ascending node: | 63.4378° |
| argument of perigee: | 234.5428° |
| revolutions per day: | 14.78765427 |
| mean anomaly at epoch: | 125.3385° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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