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 65281U 26145.58473301 +.00000000 +00000-0 +39208-3 0 00009
2 65281 97.4480 198.1142 0001870 101.7417 258.4020 15.05647389 08
| Epoch (UTC): | 25 May 2026 14:02:00 |
| Eccentricity: | 0.0001870 |
| inclination: | 97.4480° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 198.1142° |
| argument of perigee: | 101.7417° |
| revolutions per day: | 15.05647389 |
| mean anomaly at epoch: | 258.4020° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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