▸Orbital parameters

Orbit class	SSO
Inclination	97.3822°
Eccentricity	0.0004954
Period	92.6 min
Apogee	405 km
Perigee	398 km
Mean motion	15.55133860 rev/day
RAAN	276.0489°
Arg of perigee	194.8620°
Mean anomaly	165.2489°
B*	7.3541e-4
Rev at epoch	10,560

▸Two-line element set (TLE)

EPOCH Jul 7, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 60511U 24149AV 26188.15197968 .00049698 00000-0 73541-3 0 9993

2 60511 97.3822 276.0489 0004954 194.8620 165.2489 15.55133860105608

▸ source OMM (JSON)

{
  "OBJECT_NAME": "FLOCK 4BE-2",
  "OBJECT_ID": "2024-149AV",
  "EPOCH": "2026-07-07T03:38:51.044+00:00",
  "MEAN_MOTION": 15.5513386,
  "ECCENTRICITY": 0.0004954,
  "INCLINATION": 97.3822,
  "RA_OF_ASC_NODE": 276.0489,
  "ARG_OF_PERICENTER": 194.862,
  "MEAN_ANOMALY": 165.2489,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 60511,
  "REV_AT_EPOCH": 10560,
  "BSTAR": 0.00073541,
  "MEAN_MOTION_DOT": 0.00049698,
  "MEAN_MOTION_DDOT": 0
}

Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.

▸Satellite metadata

Name	FLOCK 4BE-2
Operator	Planet Labs, Inc. (Planet)HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Aug 16, 2024HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	5.7HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	PAYLOADHIGH

▸Data quality

Score85 / 100

Claims7

Sources1

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org

▸Actions

GET /api/v1/satellites/60511

//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.