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 49280U 26145.39319860 +.00000000 +00000-0 -23431-2 0 00009
2 49280 87.9178 278.9852 0001894 91.7672 268.3678 13.20761425 01
| Epoch (UTC): | 25 May 2026 09:26:12 |
| Eccentricity: | 0.0001894 |
| inclination: | 87.9178° |
| perigee height: | 1180 km |
| apogee height: | 1183 km |
| right ascension of ascending node: | 278.9852° |
| argument of perigee: | 91.7672° |
| revolutions per day: | 13.20761425 |
| mean anomaly at epoch: | 268.3678° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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