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 49284U 26145.37717995 +.00000000 +00000-0 +13827-3 0 00000
2 49284 87.9177 278.9856 0002052 101.8774 258.2590 13.20769556 05
| Epoch (UTC): | 25 May 2026 09:03:08 |
| Eccentricity: | 0.0002052 |
| inclination: | 87.9177° |
| perigee height: | 1180 km |
| apogee height: | 1183 km |
| right ascension of ascending node: | 278.9856° |
| argument of perigee: | 101.8774° |
| revolutions per day: | 13.20769556 |
| mean anomaly at epoch: | 258.2590° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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