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 48971U 26145.50156412 +.00000000 +00000-0 +25923-3 0 00008
2 48971 87.9095 233.2825 0002091 97.5455 262.5914 13.16600088 03
| Epoch (UTC): | 25 May 2026 12:02:15 |
| Eccentricity: | 0.0002091 |
| inclination: | 87.9095° |
| perigee height: | 1196 km |
| apogee height: | 1199 km |
| right ascension of ascending node: | 233.2825° |
| argument of perigee: | 97.5455° |
| revolutions per day: | 13.16600088 |
| mean anomaly at epoch: | 262.5914° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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