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LEMUR-2-KRISH

In orbit NORAD 64561 KWLN-0201-6725-2990-8850

Falcon 9

Carrier rocket

База Вандерберг

Spaceport

0

Observations all time

Mission information
Spacecraft name
LEMUR-2-KRISH
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Carrier rocket
Falcon 9
Spaceport
База Вандерберг
Launch time
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
571.89 km
Apogee
574.10 km
Inclination
97.8°
Period
96.2 min
Semi-major axis
6951.1 km
Velocity
7.56 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-09 12:46:41 UTC
Two-line elements (TLE)
1 64561U 25135AK  26281.79805453  .00003928  00000-0  34584-3 0  9997
2 64561 97.7840 36.0197 0001587 103.3692 256.7707 14.97061080 70917
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Orbit history, past year

Mean elements of every TLE set over the past 365 days, plotted against the epoch of the set. Each source is its own line; click it in the legend to hide it. A jump in altitude is a manoeuvre or a bad set; lines drifting apart are a disagreement between sources. “TLE age” is how many hours have passed since the epoch of the source's freshest set, plotted against when the set reached us, on a logarithmic scale. A set the source repeats unchanged does not reset the age.

Prediction divergence

Each TLE set is propagated with SGP4 to the epoch of the next set from the same source and compared with it, plotted against the epoch of the next set; the tooltip shows how many hours ahead the prediction ran. The logarithmic scale shows the size of the divergence and the tooltip its sign: plus along-track means the prediction is ahead of the satellite. This is how well the sets agree, not the true error: the reference is a TLE too, off by about a kilometre. An outlier is a manoeuvre between sets. Sets more than a week apart are not compared.

Time of closest approach, UTC Object 1 Object 2 Distance, km Speed, km/s Max. probability
2026-10-10 19:32:37 STARLINK-5019
NORAD 55407
LEMUR-2-KRISH
NORAD 64561
4.265 14.75 2.9e-06
2026-10-11 02:03:13 COSMOS 2583
NORAD 62904
LEMUR-2-KRISH
NORAD 64561
2.239 10.07 6.9e-07
2026-10-11 03:39:28 COSMOS 2582
NORAD 62903
LEMUR-2-KRISH
NORAD 64561
2.087 10.08 7.9e-07
2026-10-11 08:20:40 STARLINK-5508
NORAD 55639
LEMUR-2-KRISH
NORAD 64561
3.707 5.98 9.0e-06
2026-10-12 00:27:50 LEMUR-2-KRISH
NORAD 64561
STARLINK-36189
NORAD 67010
3.782 13.76 4.8e-06
2026-10-12 08:39:17 STARLINK-6029
NORAD 56803
LEMUR-2-KRISH
NORAD 64561
1.531 13.08 3.3e-05
2026-10-13 13:21:39 STARLINK-5923
NORAD 56489
LEMUR-2-KRISH
NORAD 64561
1.245 13.50 4.7e-05
2026-10-13 15:50:33 LEMUR-2-KRISH
NORAD 64561
PEGASUS DEB
NORAD 39323
4.354 15.08 8.0e-08
2026-10-13 16:39:58 BRO-15
NORAD 60553
LEMUR-2-KRISH
NORAD 64561
2.701 5.27 5.7e-07
2026-10-14 00:35:22 LEMUR-2-KRISH
NORAD 64561
STARLINK-34664
NORAD 64806
4.427 11.57 4.7e-06
2026-10-14 12:43:28 ION SCV-013
NORAD 58300
LEMUR-2-KRISH
NORAD 64561
3.286 7.56 3.6e-07
2026-10-14 16:35:51 LEMUR-2-KRISH
NORAD 64561
STARLINK-36056
NORAD 67206
4.612 8.11 5.4e-06
2026-10-14 17:38:30 SHIYAN-24C 03
NORAD 58652
LEMUR-2-KRISH
NORAD 64561
1.247 14.51 1.2e-06
2026-10-14 18:05:16 STARLINK-5071
NORAD 55402
LEMUR-2-KRISH
NORAD 64561
3.156 15.01 4.8e-06
2026-10-15 18:16:10 LEMUR-2-KRISH
NORAD 64561
DMSP 5D-2 F11 DEB
NORAD 28325
2.932 14.34 2.3e-07
2026-10-15 20:54:40 SHIYAN-24C 02
NORAD 58651
LEMUR-2-KRISH
NORAD 64561
3.869 14.51 1.3e-07
2026-10-15 23:18:59 STARLINK-3093
NORAD 49141
LEMUR-2-KRISH
NORAD 64561
4.680 7.76 5.3e-06
2026-10-15 23:18:59 SHIYAN-24C 02
NORAD 58651
LEMUR-2-KRISH
NORAD 64561
3.252 14.54 1.8e-07
2026-10-16 02:06:12 STARLINK-5623
NORAD 55405
LEMUR-2-KRISH
NORAD 64561
3.325 15.05 4.2e-06
2026-10-16 04:30:18 LEMUR-2-KRISH
NORAD 64561
SNUGLITE-III
NORAD 66661
4.856 14.98 6.7e-08
2026-10-16 12:50:21 SATELIOT_3
NORAD 60552
LEMUR-2-KRISH
NORAD 64561
2.372 5.05 7.4e-07
2026-10-17 00:10:49 SHIYAN-24C 01
NORAD 58650
LEMUR-2-KRISH
NORAD 64561
1.264 14.51 1.2e-06

Data: CelesTrak SOCRATES Plus, computed from TLEs of the public catalog. This is an estimate, not grounds for a manoeuvre: TLEs carry no covariance, and the maximum probability assumes a position error.

All conjunctions of this satellite