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 48982U 26145.53721147 +.00000000 +00000-0 +20214-3 0 00004
2 48982 87.9105 233.2815 0001982 94.1254 266.0104 13.16594082 00
| Epoch (UTC): | 25 May 2026 12:53:35 |
| Eccentricity: | 0.0001982 |
| inclination: | 87.9105° |
| perigee height: | 1196 km |
| apogee height: | 1199 km |
| right ascension of ascending node: | 233.2815° |
| argument of perigee: | 94.1254° |
| revolutions per day: | 13.16594082 |
| mean anomaly at epoch: | 266.0104° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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