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 49400U 26145.07209412 +.00000000 +00000-0 +32866-3 0 00001
2 49400 97.3257 191.2457 0009742 283.3371 76.6784 15.31191270 08
| Epoch (UTC): | 25 May 2026 01:43:48 |
| Eccentricity: | 0.0009742 |
| inclination: | 97.3257° |
| perigee height: | 466 km |
| apogee height: | 479 km |
| right ascension of ascending node: | 191.2457° |
| argument of perigee: | 283.3371° |
| revolutions per day: | 15.31191270 |
| mean anomaly at epoch: | 76.6784° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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