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 49029U 26145.42117323 +.00000000 +00000-0 +16798-3 0 00002
2 49029 34.9954 51.3874 0002767 61.2885 298.8101 15.02557065 05
| Epoch (UTC): | 25 May 2026 10:06:29 |
| Eccentricity: | 0.0002767 |
| inclination: | 34.9954° |
| perigee height: | 557 km |
| apogee height: | 561 km |
| right ascension of ascending node: | 51.3874° |
| argument of perigee: | 61.2885° |
| revolutions per day: | 15.02557065 |
| mean anomaly at epoch: | 298.8101° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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