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 48970U 26145.51266022 +.00000000 +00000-0 +79017-4 0 00001
2 48970 87.9105 233.2718 0002130 94.3378 265.7996 13.16596247 04
| Epoch (UTC): | 25 May 2026 12:18:13 |
| Eccentricity: | 0.0002130 |
| inclination: | 87.9105° |
| perigee height: | 1196 km |
| apogee height: | 1199 km |
| right ascension of ascending node: | 233.2718° |
| argument of perigee: | 94.3378° |
| revolutions per day: | 13.16596247 |
| mean anomaly at epoch: | 265.7996° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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