▸Orbital parameters

Orbit class	SSO
Inclination	97.3750°
Eccentricity	0.0003703
Period	93.4 min
Apogee	445 km
Perigee	440 km
Mean motion	15.41201300 rev/day
RAAN	271.2759°
Arg of perigee	170.7325°
Mean anomaly	189.3991°
B*	4.4899e-4
Rev at epoch	10,530

▸Two-line element set (TLE)

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

1 60481U 24149P 26188.02702595 .00018577 00000-0 44899-3 0 9999

2 60481 97.3750 271.2759 0003703 170.7325 189.3991 15.41201300105309

▸ source OMM (JSON)

{
  "OBJECT_NAME": "FLOCK 4BE-7",
  "OBJECT_ID": "2024-149P",
  "EPOCH": "2026-07-07T00:38:55.042+00:00",
  "MEAN_MOTION": 15.412013,
  "ECCENTRICITY": 0.0003703,
  "INCLINATION": 97.375,
  "RA_OF_ASC_NODE": 271.2759,
  "ARG_OF_PERICENTER": 170.7325,
  "MEAN_ANOMALY": 189.3991,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 60481,
  "REV_AT_EPOCH": 10530,
  "BSTAR": 0.00044899,
  "MEAN_MOTION_DOT": 0.00018577,
  "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-7
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/60481

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